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CRJ200Maintenance Time Limitations Manual

All Rights Reserved. Revision 1 / April 15, 2008

Maintenance Time Limitations Manual CRJ200

This Revision incorporates Revision 11 of Part 1 and Revision 7 of Part 2 of the CL-600-2B19 (CRJ 200) MRM.

Temporary Revision Part / Revision Temporary Revision Part / Revision Temporary Revision Part / Revision

1-2-34 1/11 1-2-36 1/11 2B-2134 2/7

1-2-35 1/11 2B-2126 2/7 2B-2135 2/7

1-4-1 1/11 2B-2127 2/7

1-5-2 1/11 2B-2128 2/7

1-5-3 1/11 2A-41 2/7

1-5-4 1/11 2B-2129 2/7

1-5-5 1/11 2B-2130 2/7

1-5-6 1/11 2B-2131 2/7

1-5-7 1/11 2B-2132 2/7

2B-2125 2/7 2B-2133 2/7

ii

Revision Status

Listed are the Temporary Revision's which have been incorporated into Revision 1 of the Maintenance Time Limitations Manual. The list includes the Temporary Revision Number, the Part of the MRM the TR is effective, and the Revision Number of the specified part.

Revision 1 / April 15, 2008

Maintenance Time Limitations Manual

CRJ200

Revisions to the Maintenance Time Limitations Manual will be annotated below with Revision date.

Revision No. Revision Date Revision No. Revision Date Revision No. Revision Date

0 December 11,2006 10 20

1 April 15, 2008 11 21

2 12 22

3 13 23

4 14 24

5 15 25

6 16 26

7 17 27

8 18 28

9 19 29

iii

Record of Revisions


Temporary Revision No. Issue Date Date Inserted Inserted By: Temporary

Revision No. Issue Date Date Inserted Inserted By:

TR08-01 05/08/2008 05/27/2008TR08-02 06/17/ 2008 07/09/2008

iv

The Manual Holder must record the insertion of Temporary Revisons upon receipt of the Temporary Revision.

Record of Temporary Revisions

csalsman

Rectangle


Page No. Revision / Date Page No. Revision / Date Page No. Revision / DateTitle 1 / April 15, 2008 10 1 / April 15, 2008

i 1 / April 15, 2008 9 1 / April 15, 2008 11 1 / April 15, 2008Revision Status 10 1 / April 15, 2008 12 1 / April 15, 2008

ii 1 / April 15, 2008 11 1 / April 15, 2008 13 1 / April 15, 2008Record of Revisions 12 1 / April 15, 2008 14 1 / April 15, 2008

iii 1 / April 15, 2008 13 1 / April 15, 2008 Chapter 3: Structural ProgramRecord of Temporary Revisions 14 1 / April 15, 2008 i 1 / April 15, 2008

iv 1 / April 15, 2008 15 1 / April 15, 2008 ii 1 / April 15, 2008List of Effective Pages 16 1 / April 15, 2008 1 1 / April 15, 2008

v 1 / April 15, 2008 17 1 / April 15, 2008 2 1 / April 15, 2008vi 1 / April 15, 2008 18 1 / April 15, 2008 3 1 / April 15, 2008

Revision Highlights 19 1 / April 15, 2008 4 1 / April 15, 20081 1 / April 15, 2008 20 1 / April 15, 2008 5 1 / April 15, 20082 1 / April 15, 2008 21 1 / April 15, 2008 6 1 / April 15, 20083 1 / April 15, 2008 22 1 / April 15, 2008 Chapter 4: Zonal Program4 1 / April 15, 2008 23 1 / April 15, 2008 i 1 / April 15, 20085 1 / April 15, 2008 24 1 / April 15, 2008 1 1 / April 15, 2008

Table of Contents Chapter 2: System / Powerplant 2 1 / April 15, 20081 1 / April 15, 2008 i 1 / April 15, 2008 3 1 / April 15, 20082 1 / April 15, 2008 ii 1 / April 15, 2008 4 1 / April 15, 20083 1 / April 15, 2008 1 1 / April 15, 2008 5 1 / April 15, 2008

Chapter 1: Program Description 2 1 / April 15, 2008 Chapter 5: AWL Program1 1 / April 15, 2008 3 1 / April 15, 2008 i 1 / April 15, 20082 1 / April 15, 2008 4 1 / April 15, 2008 ii 1 / April 15, 20083 1 / April 15, 2008 5 1 / April 15, 2008 1 1 / April 15, 20084 1 / April 15, 2008 6 1 / April 15, 2008 2 1 / April 15, 20085 1 / April 15, 2008 7 1 / April 15, 2008 3 1 / April 15, 20086 1 / April 15, 2008 8 1 / April 15, 2008 4 1 / April 15, 20087 1 / April 15, 2008 9 1 / April 15, 2008 5 1 / April 15, 2008

v

List of Effective Pages


List of Effective PagesPage No. Revision / Date Page No. Revision / Date

6 1 / April 15, 2008 34 1 / April 15, 20087 1 / April 15, 2008 35 1 / April 15, 20088 1 / April 15, 2008 36 1 / April 15, 20089 1 / April 15, 2008 Chapter 6: FSL

10 1 / April 15, 2008 i 1 / April 15, 200811 1 / April 15, 2008 1 1 / April 15, 200812 1 / April 15, 2008 Chapter 7: CPCP13 1 / April 15, 2008 i 1 / April 15, 200814 1 / April 15, 2008 ii 1 / April 15, 200815 1 / April 15, 2008 1 1 / April 15, 200816 1 / April 15, 2008 2 1 / April 15, 200817 1 / April 15, 2008 Chapter 8: Other Required Maintenance Tasks18 1 / April 15, 2008 i 1 / April 15, 200819 1 / April 15, 2008 1 1 / April 15, 200820 1 / April 15, 2008 2 1 / April 15, 200821 1 / April 15, 2008 3 1 / April 15, 200822 1 / April 15, 2008 4 1 / April 15, 200823 1 / April 15, 2008 5 1 / April 15, 200824 1 / April 15, 2008 6 1 / April 15, 200825 1 / April 15, 200826 1 / April 15, 200827 1 / April 15, 200828 1 / April 15, 200829 1 / April 15, 200830 1 / April 15, 200831 1 / April 15, 2008 Signature/Date32 1 / April 15, 2008 Principal Maintenance Inpsector33 1 / April 15, 2008 Federal Aviation Administration

vi

Maintenance Time Limitations Manual CRJ200Revision Highlights

MRB No./Chapter Revision Description Section

Chapter 1 Revised to remove reference to the "Aerosoft" system. Maintenance Program DescriptionChapter 1 Added the word "Change" and its definition, on page 2. Per R. 11 Part 1 MRM Maintenance Program DescriptionChapter 1 Added the word "Removal" and its definition, on page 7. Per R. 11 Part 1 MRM Maintenance Program DescriptionChapter 1 Added the acronym "WIG" to page 16. Per R. 11 Part 1 MRM. Maintenance Program DescriptionChapter 1 Revised "A Check" Note to better discribe the A check program on page 19. Maintenance Program DescriptionChapter 1 Added "FC" to verbiage of C check to page 19 and 20 to ensure table and verbiage have same meaning. Maintenance Program DescriptionChapter 1 Added to "C Check" Note that checks are unchained and interval driven on page 20. Maintenance Program DescriptionChapter 1 Revised the "C Check" to remove the calander limits per Rev. 11 Part 1 MRM. Maintenance Program DescriptionChapter 1 Added "Calander Check" program. Maintenance Program DescriptionChapter 1 Revised New Task Introduction to include Existing task revision on page 21. Maintenance Program DescriptionChapter 1 Added Program Temporary Revision language on page 22. Maintenance Program DescriptionChapter 1 Revised Program Review and Audit, replaced Mgr Mx Programs with Mgr Tech Services Maintenance Program DescriptionChapter 1 Added the Definition of "REO" Maintenance Program DescriptionChapter 1 Added the acronym for "REO". Maintenance Program DescriptionChapter 1 Added the Definition of "WIG" Maintenance Program DescriptionChapter 2 Revised Note 2 per R. 11 Part 1 MRM. System/PowerplantChapter 2 Revised Note 4 per R. 11 Part 1 MRM. System/PowerplantChapter 2 Deleted Note 7 per R. 11 Part 1 MRM. System/Powerplant21-51-21-07 Revised to add Effectivity Per TR 1-2-36. System/Powerplant21-51-21-09 Added new task Per TR 1-2-36. System/Powerplant25-17-01-01 Revised to add Note 15 per R. 11 Part 1 MRM System/Powerplant25-61-01-01-A Added task for New Part Number System/Powerplant25-61-01-01-B Added task for New Part Number System/Powerplant26-22-00-02 Added 26-22-00-02 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant26-25-00-04 Added 26-25-00-04, task reinstated per R. 11 Part 1 MRM System/Powerplant26-25-01-01 Revised Interval from 120MO to 60MO per DOT requirement. RPA tracking 60MO as of 12/27/06. No Change due to R. 11 Part 1 MRM

- notes not necessary. System/Powerplant27-15-05-01 Added 27-15-05-01 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant27-15-05-05 Added 27-15-05-05 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant27-20-00-03 Added 27-20-00-03 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant27-31-00-03 Added 27-31-00-03 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant27-34-05-01 Added 27-34-05-01 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant27-34-05-03 Added 27-34-05-03 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant27-40-01-14 Revised Interval from 8000 FH to 5500 FH per R. 11 Part 1 MRM. System/Powerplant27-50-01-07 Added 27-50-01-07 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant27-50-01-08 Added 27-50-01-08 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant30-12-12-01 Added 30-12-12-01 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant30-12-23-01 Added 30-12-23-01 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant31-41-04-01 Added 31-41-04-01 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant31-41-04-03 Added 31-41-04-03 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM System/Powerplant32-00-00-07 Task Deleted per R. 11 Part 1 MRM. System/Powerplant33-50-00-03 Task Deleted per R. 11 Part 1 MRM. System/Powerplant33-50-00-05 Added New Task 33-50-00-05 per R. 11 Part 1 MRM. System/Powerplant

Revision 1 / April 15, 2008 Revision Highlights 1 of 5



34-11-00-05 Revised Interval from 24 MO to 500FH and Revised Inspection Type from DI to GVI per R. 11 Part 1 MRM. System/Powerplant35-11-03-03 Added 35-11-03-03 from Precluded/Deleted section with Note 15 per R. 11 Part 1 MRM. System/Powerplant38-11-01-01 Added effectivity information. System/Powerplant38-21-01-01 Added effectivity information. System/Powerplant49-14-19-01 Revised Interval from 12000 FH to 15000 FH per R. 11 Part 1 MRM. System/Powerplant49-15-00-01 Revised Interval from 15000 FH/APU Change to 15000 FH / Note 4 per R. 11 Part 1 MRM System/Powerplant49-20-00-01 Added effectivity information. System/Powerplant52-00-00-19 Revised Effectivity to correct typo from Pre-Modsum TC601R14500 to Post-Modsum TC601R14500 System/Powerplant71-61-00-07 Added New Task 71-61-00-07 per R. 11 Part 1 MRM. System/Powerplant76-11-00-13 Added New Task 76-11-00-13 per R. 11 Part 1 MRM. Added Note 4 per TR 1-2-35. System/Powerplant79-21-05-03 Revised Interval from 4000 FH to 5000 FH per R. 11 Part 1 MRM. System/Powerplant53-300-06 Revised Interval from 16000 FH to 20000 FH per TR 1-4-1 R. 11 Part 1 MRM. Zonal54-400-04 Revised Interval from 24000 FH to 25000 FH per R. 11 Part 1 MRM. Zonal54-400-08 Revised Interval from 24000 FH to 25000 FH per R. 11 Part 1 MRM. Zonal55-300-10 Revised Interval from 24000 FH to 25000 FH per R. 11 Part 1 MRM. Zonal27-11-05 Task Deleted Sep 14/07 per TR 2B-2126 AWL27-11-06 Task Deleted Sep 14/07 per TR 2B-2126 AWL27-21-06 Task Deleted Sep 14/07 per TR 2B-2126 AWL27-31-02 Task Deleted Sep 14/07 per TR 2B-2126 AWL27-51-10 Revised Note to include how life limit is tracked. AWL27-54-15a Deleted from MTLM and transferred to SDIR per Rev. 7 Part 2 MRM. AWL32-11-110a Revised Note per Rev. 7 Part 2 MRM. AWL32-11-110b Revised Note per Rev. 7 Part 2 MRM. AWL32-11-110c Revised Note per Rev. 7 Part 2 MRM. AWL32-11-110d Revised Note per Rev. 7 Part 2 MRM. AWL32-11-110e Revised Note per Rev. 7 Part 2 MRM. AWL32-11-110f Revised Note per Rev. 7 Part 2 MRM. AWL49-20-01 Added effectivity information. AWL49-20-02 Added effectivity information. AWL52-11-101a Revised task number due to addition of SDI, Added Effectivity per Rev. 7 Part 2 MRM. AWL52-11-101b Added New Task per Rev. 7 Part 2 MRM. AWL52-11-102 Revised Description, Added Effectivity per Rev. 7 Part 2 MRM. AWL52-11-104a Revised task number due to addition of SDI, Revised Interval per Rev. 7 Part 2 MRM. AWL52-11-104b Added New Task per Rev. 7 Part 2 MRM. AWL52-11-105 Revised Interval per Rev. 7 Part 2 MRM. AWL52-11-131 Added New Task per Rev. 7 Part 2 MRM. Revised Phase-in per TR 2B-2127. AWL53-11-122a Revised Task Number, Description, and Interval. Added Effectivity and Phase-in statement per Rev. 7 Part 2 MRM. AWL53-11-122b Added New Task per Rev. 7 Part 2 MRM. AWL53-21-102 Added Note and revised repeat interval per TR 2B-2129 of Rev. 7 Part 2 MRM. AWL53-21-103 Revised Interval and Added Effectivity per Rev. 7 Part 2 MRM. AWL53-21-115 Revised Threshold and Repeat Intervals and added Note per TR 2B-2129 of Rev. 7 Part 2 MRM. AWL53-21-118 Revised Threshold Interval and added Note per TR 2B-2129 of Rev. 7 Part 2 MRM. AWL53-21-127 Revised Repeat Inspection Interval and added Note per TR 2B-2128 AWL53-21-128 Revised Interval per Rev. 7 Part 2 MRM. AWL




53-21-129 Added New Task per Rev. 7 Part 2 MRM. Revised Phase-in per TR 2B-2128 AWL53-41-119 Added Phase-in statement and Note per TR 2B-2132 Rev. 7 Part 2 MRM. AWL53-41-138-2 Revised Interval per Rev. 7 Part 2 MRM. AWL53-41-159-1 Added Phase-in statement per TR 2B-2130 Rev. 7 Part 2 MRM. AWL53-41-159-2 Added Phase-in statement per TR 2B-2130 Rev. 7 Part 2 MRM. AWL53-41-163 Added Note and revised Threshold and Repeat Interval per TR 2B-2130 of Rev. 7 Part 2 MRM. AWL53-41-193 Revised Effectivity per Rev. 7 Part 2 MRM. AWL53-41-194 Revised Description, Interval, and Effectivity per Rev. 7 Part 2 MRM. AWL53-41-195 Revised Description and Effectivity per Rev. 7 Part 2 MRM. AWL53-61-153a Revised Notes to include Chautauqua's choice of inspection method per Note 4. AWL53-61-153b Revised Notes to include Chautauqua's choice of inspection method per Note 4. AWL54-10-105 Revised Threshold and Repeat Intervals added Phase-In statement and Note per TR 2B-2133 of Rev. 7 Part 2 MRM. AWL54-10-106 Revised Threshold and Repeat Intervals per TR 2B-2133 of Rev. 7 Part 2 MRM. AWL57-21-105 Added Phase-In statement and Note per TR 2B-2134 Rev. 7 Part 2 MRM. AWL57-21-112 Added Note per TR 2B-2134 Rev. 7 Part 2 MRM. AWL57-21-115 Revised Threshold Interval and added Note per TR 2B-2131 of Rev. 7 Part 2 MRM. AWL57-21-130-2 Revised Interval per Rev. 7 Part 2 MRM. AWL57-21-146 Repeat Interval reduced to lowest interval permissible per TR 2B-2125 of Part 2 MRM for REO 601R-57-21-030 NC A, B, C, D. AWL57-21-147 Repeat Interval reduced to lowest interval permissible per TR 2B-2125 of Part 2 MRM for REO 601R-57-21-030 NC A, B, C, D. AWL57-21-148 Repeat Interval reduced to lowest interval permissible per TR 2B-2125 of Part 2 MRM for REO 601R-57-21-030 NC A, B, C, D. AWL57-21-149 Repeat Interval reduced to lowest interval permissible per TR 2B-2125 of Part 2 MRM for REO 601R-57-21-030 NC A, B, C, D. AWL57-21-150 Revises Effectivity statement to include CHQ's option. AWL57-21-151 Revised Note 3 per Rev. 7 Part 2 MRM. AWL57-52-108 Revised Interval per Rev. 7 Part 2 MRM. AWL57-53-125 Added New Task per Rev. 7 Part 2 MRM. Added Effectivity Per TR 2B-2135 of Rev. 7 Part 2 MRM. AWLC21-50-115-01 Revised interval from 8000 FH to 10000 FH per TR 2A-31. AWLC25-17-152-01 Revised interval from 4000 FH to 5000 FH per TR 2A-31. AWLC26-10-131-01 Revised interval from 8000 FH to 10000 FH per TR 2A-31. AWLC27-10-105-01 Revised interval from 800 FH to 1000 FH per TR 2A-31. AWLC27-10-105-03 Revised interval from 8000 FH to 10000 FH per Rev. 7 MRM Part 2. AWLC27-10-105-05a Revised interval from 4000 FH to 5000 FH per Rev. 7 MRM Part 2. AWLC27-10-105-05b Revised interval from 4000 FH to 5000 FH per Rev. 7 MRM Part 2. AWLC27-10-105-07 Revised interval from 4000 FH to 5000 FH per Rev. 7 MRM Part 2. AWLC27-20-108-01 Revised interval from 8000 FH to 10000 FH per Rev. 7 MRM Part 2. AWLC27-30-102-01 Revised interval from 8000 FH to 10000 FH per Rev. 7 MRM Part 2. AWLC27-30-102-03 Revised interval from 4000 FH to 5000 FH per Rev. 7 MRM Part 2. AWLC27-30-102-05 Revised interval from 8000 FH to 10000 FH per Rev. 7 MRM Part 2. AWLC27-35-112-01 Revised interval from 4000 FH to 5000 FH per TR 2A-32. AWLC27-40-103-01 Deleted Task per TR 2A-32. AWLC27-50-111-01 Revised Interval from 3500 FH to 1000 FH and Effectivity per TR 2A-37 part 2 MRM. AWLC27-50-111-03 Revised Interval from 8000 FH to 500 FH and Effectivity per TR 2A-37 part 2 MRM. AWLC27-50-111-06 Revised Task Description, Inspection Type, and Effectivity per TR 2A-38 Part 2 MRM. AWLC27-50-111-07 Revised Interval from 500 FH to 1000 FH and Effectivity per TR 2A-38 Part 2 MRM. AWLC27-50-111-09 Revised Interval from 500 FH to 1000 FH and Effectivity per TR 2A-39 Part 2 MRM. AWL




C27-50-111-10 Revised Effectivity per TR 2A-39 Part 2 MRM. AWLC27-50-111-11 Revised Interval from 10000 FH to 10666 FH and Effectivity per TR 2A-39 Part 2 MRM. AWLC27-50-111-12 Added Task per TR 2A-40 Part 2 MRM. AWLC27-50-300-01 Added Task per TR 2A-41 Part 2 MRM. AWLC27-60-106-01 Revised interval from 800 FH to 1000 FH per Rev. 7 Part 2 MRM. AWLC28-20-131-01 Revised Interval from 4000 FH to 5000 FH per TR 2A-35. AWLC31-40-158-01 Revised Interval from 4000 FH to 5000 FH per TR 2A-35. AWLC34-40-107-01 Revised Description, Interval from 8000 FH to 10000 FH, and added Effectivity per TR 2A-36. AWLC35-10-128-01 Revised Interval from 400 FH to 500 FH per TR 2A-36. AWLC36-20-133-01 Revised Interval from 400 FH to 500 FH per TR 2A-36. AWLC36-20-133-02 Revised Interval from 400 FH to 500 FH per TR 2A-36. AWLC52-10-821-01 Revised ETOPS/CMR/AD column to remove CMR status as this task is not a CMR. AWLR27-31-A024-01 Task Deleted per Rev. 7 Part 2 MRM. AWLREO 601R-53-00-061 A Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-11-162 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-21-180 NC-1 Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-21-180 NC-2 Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-21-183 NC-1 Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-21-183 NC-2 Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-21-313 NC-1 Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-21-313 NC-2 Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-31-012 C or D-1 Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-31-012 C or D-2 Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-31-019 NC to C Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-41-010 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-41-057 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-41-067 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-41-102 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-53-41-103 A Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-55-11-061 NC-a Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-55-11-061 NC-b Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-55-21-080 NC-a Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-55-21-080 NC-b Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-55-21-082 NC-a Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-55-21-082 NC-b Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-57-21-030 NC A, B, C, D

Add REO 601R-57-21-030 NC A, B, C, D per TR-2B-2125 of Part 2 MRM.AWL

REO 601R-57-21-037 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-57-21-046 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-57-21-169 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-57-61-004 B Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWLREO 601R-57-61-052 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM. AWL28-11-00-601 Revised to add Effectivity per Rev. 7 Part 2 MRM. FSL28-11-00-602 Revised to add Effectivity per Rev. 7 Part 2 MRM. FSL




28-11-00-604 Added New Task 28-11-00-604 per TR 2D-4 Part 2 MRM and Added Effectivity per Rev. 7 Part 2 MRM. FSL52-11-03-01 Revised Threshold interval to 72 MO from 96 MO per TR 1-5-2. CPCPChapter 8 Revised Introduction to Chapter 8 to include statement for AD Summary. Other Required Maintenance ItemsAD 2004-10-03 Revised Interval to correct value Other Required Maintenance ItemsAD 2004-14-16 AD superceded by AD 2007-03-19 Other Required Maintenance ItemsAD 2004-14-16 AD superceded by AD 2007-03-19 Other Required Maintenance ItemsAD 2004-14-16 AD superceded by AD 2007-03-19 Other Required Maintenance ItemsAD 2004-14-16 AD superceded by AD 2007-03-19 Other Required Maintenance ItemsAD 2004-20-09 AD superceded by AD 2007-01-07 Other Required Maintenance ItemsAD 2004-20-09 AD superceded by AD 2007-01-07 Other Required Maintenance ItemsAD 2004-20-09 AD superceded by AD 2007-01-07 Other Required Maintenance ItemsAD 2004-20-09 AD superceded by AD 2007-01-07 Other Required Maintenance ItemsAD 2005-17-12 Revised RPA tracking task numbers Other Required Maintenance ItemsAD 2005-17-12 (terminating Action)

Added Terminating Action Other Required Maintenance Items

AD 2006-10-01 Revised RPA tracking task from 061001B to 061001D Other Required Maintenance ItemsAD 2006-10-06 Added AD Other Required Maintenance ItemsAD 2007-01-07 Added New AD, this AD suppercedes AD 2004-20-09. Other Required Maintenance ItemsAD 2007-01-07 Added New AD, this AD suppercedes AD 2004-20-09. Other Required Maintenance ItemsAD 2007-01-07 Added New AD, this AD suppercedes AD 2004-20-09. Other Required Maintenance ItemsAD 2007-01-07 Added New AD, this AD suppercedes AD 2004-20-09. Other Required Maintenance ItemsAD 2007-01-07 (Terminating Action)

Added Terminating Action Other Required Maintenance Items

AD 2007-03-19 Added New AD, this AD suppercedes AD 2004-14-16. Other Required Maintenance ItemsAD 2007-03-19 Added New AD, this AD suppercedes AD 2004-14-16. Other Required Maintenance ItemsAD 2007-03-19 Added New AD, this AD suppercedes AD 2004-14-16. Other Required Maintenance ItemsAD 2007-03-19 Added New AD, this AD suppercedes AD 2004-14-16. Other Required Maintenance ItemsAD 2007-04-24 Added New AD Other Required Maintenance ItemsAD 2007-04-24 Added New AD Other Required Maintenance ItemsAD 2007-07-07 Added New AD. Other Required Maintenance ItemsAD 2007-15-02 Added New AD. Other Required Maintenance ItemsAD 2007-15-02 Added New AD. Other Required Maintenance ItemsAD 2007-15-02 Added New AD. Other Required Maintenance ItemsAD 2007-15-02 Added New AD. Other Required Maintenance ItemsAD 2008-06-10 Added New AD. Other Required Maintenance Items



Chapter 1: Maintenance Program Description…………………… 1Introduction…………………… 1Definition of Terms…………… 2Abbreviations………………… 10Program Overview…………… 17

Systems/Powerplant Program…………………………… 17Zonal Inspection Program………………………………… 17Structural Inspection Program…………………………… 17

Program Outline……………… 19Line Checks……………… 19"A" Checks………………… 19"C" Checks………………… 19Computer controlled Tasks………………………………. 20Weighing…………………………………………………… 20High Pressure Bottle Hydrostatic Test…………………. 20Fuel System Limitations…………………………………… 20Escalation or De-escalation of Maintenance Time Intervals…………………………………………………………………21

21Maintenance Short Term Escalation Policy……………………………………………………………………………………21Unscheduled Events……… 21Maintenance Time Limits Manual Format…………………………………………………………………………………… 21Appendix………………………………………………...……………………………………… ………………………………. 21

Miscellaneous Program Information…………………………… 22Program Revisions……… 22Program Temporary Revision………………………………………………………………………………………………… 22Program Review and Audit………………………………… 23

Master Table of Contents……………………………………………………………………

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New Task Introduction / Existing task revision…………………………………………………………..……………….

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1 of 3

Maintenance Time Limitations Manual CRJ200Master Table of Contents

Chapter 2: Systems/Powerplant Program………………………… iIntroduction…………………… i

Program Notes…………… iFormat……………………… ii

Table………………………………………………………………………………………………… ……………………………… 1

Chapter 3: Structural Program…… iIntroduction…………………… i

Program Notes…………… iFormat……………………… i

Table………………………………………………………………………………………………… ……………………………… 1

Chapter 4: Zonal Maintenance Program………………………… iIntroduction…………………… i


Table………………………………………………………………………………………………… ……………………………… 1

Chapter 5: AWL Program………… iIntroduction…………………… i


Table………………………………………………………………………………………………… ……………………………… 1

Chapter 6: FSL Maintenance Program…………………………… iIntroduction…………………… i

Format……………………… iTable………………………………………………………………………………………………… ……………………………… 1

Chapter 7: CPCP Program……… iIntroduction…………………… iCorrosion Levels…………………………………………………………………………………… ………………………………. i

Format……………………… iiTable………………………………………………………………………………………………… ……………………………… 1

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2 of 3

Maintenance Time Limitations Manual CRJ200Master Table of Contents

Chapter 8: Other Required Maintenance Tasks………………… iIntroduction…………………… i

Format……………………… iTable………………………………………………………………………………………………… ……………………………… 1

Appendix A: Other Maintenance Items…………………………… iIntroduction…………………… i

Format……………………… iTable………………………………………………………………………………………………… ……………………………… 1

Appendix B: Precluded/Deleted…………………………………… iIntroduction…………………… i

Format……………………… iTable………………………………………………………………………………………………… ……………………………… 1

Appendix C: MTL No./Job Card/Check Cross Reference……… iIntroduction…………………… i

Format……………………… iTable………………………………………………………………………………………………… ……………………………… 1

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Chapter 1Maintenance Program Description

Page 1Revision 1 / April 15, 2008 CRJ200

Maintenance Program Description

IntroductionThe Maintenance Time Limits Manual (MTLM) is part of the Chautauqua Airlines Maintenance Manual system and contains comprehensive scheduled maintenancechecks that will ensure the continued airworthiness of the Canadair CL600-2B19 Airframe, Systems, Powerplant and Components. The MTLM (referred to hereafter asthe “Maintenance Program”) is applicable to the Chautauqua Airlines (referred to hereafter as “the Company”) fleet of Canadair CL600-2B19 aircraft.

The Maintenance Program tasks and intervals are derived from the Canadair CL600-2B19 Maintenance Requirements Manual (MRM), Part 1 Maintenance ReviewBoard Report (MRBR) and Part 2 Airworthiness Requirements. Additional elements have been added to facilitate the accomplishment of tasks associated withAirworthiness Directives (A.D.s), Engineering Orders (EOs) and other items identified through the Company’s Continuous Analysis and Surveillance Program.

In addition to this manual, elements of the Continuous Airworthiness Maintenance Program are contained within the Chautauqua Airlines General Maintenance Manual(GMM). The following items are described in detail within the Chautauqua Airlines GMM; Inspection Organization, Scheduled Maintenance, Overhaul and Repair,Structural Inspection, Required Inspection Items, Reliability and Continuous Analysis and Surveillance System (CASS), Calibration of Tools and Recordkeeping.

This maintenance program consists of Line Checks, A Checks and C Checks and their multiples. Additionally, there are checks that cover flight hour items, flight cycleitems, unscheduled event items, calendar and non-periodic items.

Any discrepancies noted during a check are recorded on Non Routine cards. All forms generated during a check become part of the work package and kept on file inaccordance with the records retention policy outlined in the GMM. Discrepancies noted during Line Checks, that are not part of the workscope, and other non-routinemaintenance items occurring during routine operations are recorded in the Aircraft Flight/Maintenance Log and worked in accordance with approved procedurespertaining to the type of maintenance activity involved.

The Aircraft and its component parts, accessories, and appliances shall be maintained in an airworthy condition in accordance with this document and the ChautauquaAirlines General Maintenance Manual, with regards to the accomplishment of the Maintenance tasks, periodic inspections, and routine checks. The MaintenanceProgram tasks will be accomplished using Maintenance Job Cards as described in the Company CRJ 200 Job Card Manual and the procedures contained within theCanadair CL600-2B19 Aircraft Maintenance Manual (AMM) CSP A-001, and the General Electric CF34 Engine Manual (SEI-756).

To maintain the current status of Scheduled Inspections and Checks, Life Limited Parts, and Appliance Overhaul requirements, Chautauqua Airlines employs acomputerized Time Control System. The maintenance checks, tasks, intervals, and time limitations specified in this manual are processed into the computer trackingsystem by Maintenance Program Specialists to enable effective and accurate tracking and control of the program requirements. Engineering is responsible for settingup of effectivity, applicabiliity and limitations for engines, accessories, and components.

All revisions to this manual require approval from the Certificate Holding District Office (CHDO). Revisions will be based upon analysis and/or changes of the followingdata: Airframe, Engine and Appliance performance data, inspection findings, and/or changes to OEM limitations, Certification Maintenance Requirements, MaintenanceReview Board Report, Airworthiness Directives (as applicable), Alteration Data (as applicable), and Repair Data (as applicable). Analysis and approval procedures arespecified in the Chautauqua Airlines General Maintenance Manual. A list of effective pages is provided with this document as a means of maintaining an up-to-dateInspection Program. Upon receipt of revised pages, the list should be used as a cross-reference for inserting new data. Obsolete data will be destroyed and theInspection Program will be maintained current at all times.



Definition of TermsAccidental Damage (AD)

Physical deterioration of an item caused by contact or impact with an object or influence which is not a part of the aircraft, or by human error during manufacturing,operation of the aircraft, or maintenance practices.

Age Exploration

A systematic evaluation of an item based on analysis of collected information from in-service experience. It assesses the item's resistance to a deterioration processwith respect to increasing age.

Airworthiness Limitations (AWL)

Instructions that contain each mandatory replacement time, structural inspection interval, and related structural inspection procedure. This section may also be used todefine a threshold for the fatigue-related inspection.

Calendar Time (DY, WK, MO, YR)

Day (DY): A period of time commencing at midnight, and ending the following midnight. When used as a measuring unit, it is used in whole numbers.

• Example: A task having a repeat interval of 1 DY, when accomplished at any point in Day 1, is due to be repeated at any point during the following day (day 2).

Week (WK): A period of time consisting of 7 consecutive days.

• Example: A task having an interval of 1 week, when accomplished at any point in Day 1, is due to be repeated at any point during Day 8.

Month (MO): A period of time consisting of 30 consecutive days.

Year (YR): A Period of time consisting of 12 consecutive months.

Certification Maintenance Requirements (CMR)

A CMR is a mandatory recurring check of an airplane system or component to detect the presence of, and thereby limit the exposure time to, a significant latent failurethat would, in combination with one or more specific failures or events identified in a safety analysis, result in a hazardous failure condition. CMR tasks are identified inthis document by the placement of a CMR in the CMR/AD column.

Change

A part serial number is removed from the aircraft and replaced with a part bearing a different serial number or other with another unique individual item if not serialized.

Check/Inspection (VIS, INS)

An examination of an item against a specific standard.

Cycle (CY)

A flight regime from takeoff through landing.



Damage Tolerant

A qualification standard for aircraft structure. An item is judged to be damage tolerant if it can sustain damage and the remaining structure can withstand reasonableloads without failure or excessive structural deformation until the damage is detected.

Detailed Visual Inspection (DVI)

An intensive visual examination of a specified detail, assembly, or installation. It searches for evidence of irregularity using adequate lighting and, where necessary,inspection aids such as mirrors, hand lens, etc. Surface cleaning and elaborate access procedures may be required.

Discard (DIS)

The removal from service of an item at a specified life limit.

Direct Adverse Effect on Operating Safety

Direct

To be direct the functional failure or resulting secondary damage must achieve its effect by itself, not in combination with other functional failures (no redundancyexists and it is a primary dispatch item).

Adverse Effect on Safety

This implies that the consequences are extremely serious or possibly catastrophic and might cause the loss of aircraft or injury to occupants.

Operating

This is defined as the time interval during which passengers and crew are on board for the purpose of flight.

Economic Effects

Failure effects which do not prevent aircraft operation, but are economically undesirable due to added labor and material cost for aircraft or shop repair.

Engine Cycle

An Engine Cycle is defined as a flight consisting of an acceleration to takeoff power, takeoff and landing. The use, (or non-use) of thrust reverser does not change thecycle count. Other operational procedures that affect the life limit cycles of rotating components are counted as follows:

• An air start performed for pilot training counts as one cycle for each rotating part.

• Each flight (takeoff and landing) counts as one cycle regardless of whether or not the engines are shut down prior to the next takeoff

• A touch-and-go landing counts as one cycle for each rotating part

• A go-around counts as two cycles for each rotating part if APR power is set using the throttle during the go-around (if APR power is not set, the go-aroundcounts as one cycle for each rotating part)

• Whenever the throttle is used to set APR power, 2 cycles are added to the cycle count for each rotating part



Environmental Damage/Deterioration (ED)

Physical deterioration of an item’s strength or resistance to failure as a result of chemical interaction with its climate or environment.

External Surveillance

A visual examination of defined external structural areas from a distance considered necessary to carry out an adequate check. It may include internal structure whichis visible through quick opening access panels/doors. Workstands, ladders, etc. may be required to gain proximity.

Fail Safe

A design criterion which requires that predictable failure of an item will not place the aircraft into an uncontrollable condition.

Failure

The inability of an item to perform within previously specified limits.

Failure Cause

Why the functional failure occurs.

Failure Effect

The result of a failure.

Fatigue Damage (FD)

The initiation of a crack or cracks due to cyclic action and the subsequent propagation.

Fatigue Related Sampling Program

Inspections on specific aircraft selected from those which have the highest operating age/usage in order to identify the first evidence of deterioration in their conditioncaused by fatigue damage.

Flight Cycles/Landing (FC)

A flight regime from takeoff through landing.

Flight Hours (FH)

The period of time from weight-off-wheels and weight-on-wheels.

Flight Day

“Flight Day” means a 24 hour period (from midnight to midnight) local time, during which at least one flight is initiated for the affected aircraft.



Function

The normal characteristic actions of an item.

Functional Check/Test (FNC)

A functional check verifies that a system or component functions within the limits described in the aircraft maintenance or component maintenance manual. It seesmeasurements, tests or other means to determine system or component health.

Functional Failure

How an item failed to perform its function.

General Visual Inspection (GVI)

A visual examination that will detect obvious unsatisfactory condition/discrepancies. This type of inspection may require removal of fillets, fairings, access panels/doors,etc. Workstands, ladders, etc. may be required to gain proximity.

Hidden Function

A function which is normally active and whose cessation will not be evident to the operating crew during performance of normal duties.

A function which is normally inactive and whose readiness to perform, prior to it being needed, will not be evident to the operating crew during performance of normalduties.

Inherent Level of Safety and Reliability

That level which is built into the unit and therefore inherent in its design. This is the highest level of reliability and safety that can be expected from a unit, system, oraircraft if it receives effective maintenance. To achieve higher levels of reliability generally requires modification or redesign.

Inspection (INSP)

An examination of the item against a specific standard.

Internal Surveillance

A visual examination of defined internal structural areas from a distance considered necessary to carry out an adequate check. This type of inspection applies to structureand installations which may require removal of fillets, fairings, access panels/doors, etc.

Item

A level of hardware assembly (i.e. system, subsystem, module, accessory, component, unit, part, etc.).

Line Check (LC)

Line Checks consist of tasks that can be performed during normal gate operations. These checks may also be performed during overnight maintenance at outstationsand Chautauqua Airlines maintenance bases.



Lubrication and Servicing (LUB)

Any act of lubricating or servicing for the purpose of maintaining inherent design capabilities.

Maintenance Significant Item (MSI)

Items identified by the manufacturer whose failure:

• Could affect safety (on ground or in flight), and/or

• Is detectable during operations, and/or

• Could have significant operational impact, and/or

• Could have significant economic impact.

Multiple Site Fatigue Damage

The presence of secondary damage (cracking) dependent or independent of the primary damage (crack).

MSG-3

Airline/Manufacturer maintenance program planning document prepared using MSG-3, Revision 2001.1, process and logic.

This MSG-3 analysis procedure presents a means for developing a maintenance program, outlining the general organization and decision for determining scheduledmaintenance requirements.

On-Condition

A periodic inspection or check process that is used to determine the continued serviceability of a unit that does not have a hard time overhaul and is repaired oroverhauled only when it fails to meet required physical standards. The period between inspections or checks will be expressed as hard time.

Operating Crew Normal Duties

Operating Crew - Qualified cockpit and cabin attendant personnel who are on duty.

Normal duties - Those duties associated with the routine operation of the aircraft, on a daily basis, to include the following:

• Procedures and checks performed during aircraft operation

• Recognition of abnormalities or failures by the operating crew through use of normal physical senses (e.g., odor, noise, vibration, temperature, visualobservation of damage or failure, changes in physical input force requirements, etc.).

Operational Check (OPC)

An operational check is a task to determine that an item is fulfilling its intended purpose. Does not require quantitative tolerances. This is a failure finding task.



Operational Effects

Failure effects which interfere with the completion of the aircraft mission. These failures cause delays, cancellations, ground or flight interruptions, high drag coefficients,altitude restrictions, etc.

Other Structure

Structure which is judged not to be a Structural Significant Item. “Other Structure” is defined both externally and internally within zonal boundaries.

Out-of-Service

Out-of-service is a period when an aircraft is awaiting or undergoing Modification, Repair or Storage. The aircraft cannot be dispatched for flight until the functionsmentioned have been completed and the aircraft is returned to service in the aircraft log book. During the Out of Service phase, specified scheduled maintenanceintervals, flight hours and flight cycles are stopped and will not be started again until the aircraft is returned to service.

Overhaul

Required maintenance on an aircraft, aircraft engine, appliance, or component part that has been disassembled, cleaned, inspected, repaired as necessary,reassembled, and tested in accordance with approved standards and technical data acceptable to the Administrator.

Piece-Part Exposure (as it applies to AD 2000-03-03R1)

Piece-part exposure is defined in CF34 Engine Manual SEI-756, Chapter 5-21-00. Table 804 “Mandatory Inspection Requirements” identifies inspections that must beaccomplished on specific piece-parts upon exposure. The inspection requirements referenced in Table 804 are not required for any piece-part exposure during “on-wing” maintenance, while performing Special Procedure #41, listed in SEI-756, Chapter 72-00-00. Engines which are not installed on an aircraft, and undergo piece-part exposure (fan disc piece part is defined as the fan disk with 56 fan pin bushings installed), must comply with the inspection requirements of Table 804, unless thefan disk has accumulated less than 100 cycles-in-service, is not damaged, and was not related to the cause for its removal from the engine.

Removal

A part is removed and is either re-installed or another unique part (bearing a different serial number if serialized) is installed.

Repair Engineering Order (REO)

Bombardier created repair with structural limitations. These repairs are created for structural damage during production or fleet operation. Only Aircraft that havesustained the specific damage of the repair will have these limitations tracking.

Repeat

The specific value of a usage parameter (landings, flight hours, etc.) at which the follow on inspection of some particular level or method should be conducted.

Residual Strength

The strength of a damaged structure.

Restoration (RST)

That work necessary to return the item to a specific standard. Restoration may vary from cleaning or replacement of single parts up to a complete overhaul.



Safe Life Structure

Structure which is not practical to design or qualify as damage tolerant. Its reliability is protected by discard limits which remove items from service before fatigue crackingis expected.

Scheduled Maintenance Check

Any of the maintenance opportunities which are prepackaged and are accomplished on a regular basis.

Special Detailed Inspection (SDI)

An intensive examination of a specific location similar to the detailed inspection except for the following difference; the examination requires some special techniquesuch as non-destructive test techniques, dye penetrant, high-powered magnification, etc. It may require disassembly procedures.

Structural Assembly

One or more structural elements which together provide a basic structural function structural detail. The lowest functional level in an aircraft structure. A discrete regionor area of a structural element, or a boundary intersection of two or more elements.

Structural Detail

The lowest functional element in an aircraft structure. A discrete region or area of a structural element, or a boundary intersection of two or more elements.

Structural Element

Two or more structural details which together form an identified manufacturer's assembly part.

Structural Function

The mode of action of aircraft structure. It includes acceptance and transfer of specified loads in items (details/elements/assemblies) and provides consistently adequateaircraft response and flight characteristics.

Structural Significant Item (SSI)

Any detail, element or assembly, which contributes significantly to carrying flight, ground, pressure, or control loads and whose failure could affect the structural integritynecessary for the safety of the aircraft.

Tasks - Maintenance

An action or set of actions required to achieve a desired outcome which restores an item to or maintains an item in serviceable condition, including inspection anddetermination of condition.

To Be Determined (TBD)

To Be Determined (TBD) will be used within the TLM for items such as Threshold/Repeat Values, Job card Numbers and/or Scheduled Intervals where no informationis yet available from the manufacturer and/or vendor. These TBD task will be replaced with the appropriate data when available.



Threshold

The specific value of a usage parameter (landings, flight hours, etc.) at which the first inspection of some particular level or method should be conducted.

Time Limits

Approved time limits for inspections, maintenance and overhaul of the aircraft, its systems and units, and life of parts.

Unscheduled Maintenance Inspection / Checks

Unscheduled maintenance checks and inspections on the aircraft, its systems, and units which are dictated by special or unusual conditions, which are not related tothe time limits specified above. This includes inspections and checks such as hard landing, turbulent air, lightning strike, overweight landing, bird strike, slush ingestion,radioactive contamination, etc.

Visual Check (VIS)

A visual check is an observation to determine that an item is fulfilling its intended purpose. Does not require quantitative tolerances. This is a failure finding task.

Walk Around Inspection/Check

A visual check conducted from ground level to detect obvious discrepancies.

Whichever is Greater (WIG)

If a task has two different intervals the greater of the two can be used.

Zonal Inspection

A visual inspection that may require a lamp and mirror. The surveillance is valid for all items contained within the affected zone. Unless otherwise indicated, the wholeof the zones, as visible, are to be inspected from normal viewing distance, i.e., in most cases from within a distance of one arms length.



AbbreviationsA

A/C Aircraft A/P AutopilotAAS Anti-Ice Advisory AC Advisory Circular1

AC Alternating Current1 ACARS Airborne Communications Addressing and Reporting System

ACU Air Conditioning Unit

ACM Air Cycle Machine A.D. Airworthiness Directive1

AD Accidental Damage1 ADA Accidental Damage Analysis

ADC Air Data Computer ADG Air Driven GeneratorA/D Analog to Digital ADIRU Air Data Inertial Reference UnitADF Automatic Direction Finder ADI Attitude Deviation IndicatorADS Air Data System AEG Aircraft Evaluation UnitAEU Audio Electronic Unit AEP Age Exploration ProgramAFCS Automatic Flight Control System AFT Rear LocationAH APU Operating Hours AHC AHRS ComputerAHM Altitude Hold Mode AHRS Attitude Heading Ref SystemAMM Aircraft Maintenance Manual AMTOSS Aircraft Maintenance Task Oriented Support SystemAMP Ampere AOA Angle of AttackAOG Aircraft on Ground AOM All Operators MessageAP/EP Aux Power/External Power APR Automatic Power ReserveAPS Autopilot System APU Auxiliary Power UnitAPU CNG Auxiliary Power Unit Change ARINC Aeronautical Radio Inc.ASB Alert Service Bulletin ASCB Avionics Standard Communication BusATA Air Transport Association ATC Autopilot Trim Computer1

ATC Air Traffic Control1 ATT Attitude

ATS Air Turbine Starter ATPCS Automatic Take-off Power Control SystemAWL Airworthiness Limitation

BBC Back Course BITE Built-in Test EquipmentBL Buttock Line BO BorescopeBV Bureau Veritas BTMS Brake Temp Monitoring System

1 Examine context of usage to determine which term is applicable



CC Celsius CA CalendarCAA Chromic Acid Anodizing CAM Canadian Airworthiness ManualCAC Crew Alerting Computer CADC Central Air Data ComputerCAS Crew Alerting System CAS 1 Calibrated Air SpeedCDH Clearance Delivery Head CC Conversion CoatingCHDO Certificate Holding District Office CDU Control Display UnitCMR Certification Maintenance Requirement CMM Component Maintenance ManualCRES Corrosion Resistant Steel CPI Cabin Pressure IndicatorCSD Constant Speed Drive CRT Cathode Ray TubeCVR Cockpit Voice Recorder CSDB Collins Serial Data BusCY Cycles/Landings CTR Center

DD/A Digital/Analog DADC Digital Air Data ComputerDADS Digital Air Data System DAU Data Acquisition UnitDBU Data Base Unit DC Direct CurrentDCP Display Control Panel DCU Data Concentrator UnitDEI Display Electronic Interface DFGS Digital Flight Guidance SystemDG Directional Gyro DH Decision HeightDME Distance Measuring Equipment DOT Department of TransportDR Dead Reckoning DS, DIS Discard/Replace TaskDTA Damage Tolerance Analysis DTR Damage Tolerance RatingDVI, DI Detailed Inspection DIS DiscardDU Display Unit DWR Digital Weather Radar

EE/E Electrical/Electronic EADI Electronic Attitude Director IndicatorEC Engine Change EN CHG Engine Change1

ECM Electronic Control Module ECTM Engine Control Trend MonitoringECP EICAS Control Panel ECS Environmental Control System ECO Engineering Change Order ECU Electronic Control UnitEDA Environmental Deterioration Analysis EDCU Engine Data Concentrator UnitEDP Engine Driven Pump ED Environmental Deterioration/DamageEFD Electronic Flight Display EFIS Electronic Flight Information SystemEFH Engine Flight Hour EFR Estimated Fuel RemainingEGT Exhaust Gas Temperature EHIS Electronic Horizontal Situation IndicatorEIA Electronic Industries Association EICAS Engine Indication and Crew Alert SystemELT Emergency Locator Transmitter ENG Engine




E (cont’d)EMI Electromagnetic Interference ESD Electrostatic DischargeETA Estimated Time of Arrival ETD Estimated Time of Departure

FF Fahrenheit FAR Federal Aviation RegulationsFADEC Full Authority Digital Engine Control FC Flight Cycle/Landing1

FC Functional Check1 FCP Flight Control Panel

FCC Flight Control Computer FCU Fuel Control UnitFCS Flight Control System FDA Fatigue Damage AnalysisFD Fatigue Damage FDGS Flight Director Guidance SystemFDAU Flight Data Acquisition Unit FDR Flight Data RecorderFH Flight Hour(s) FF Fuel FlowFDS Flight Director System FLC Flight Level ChangeFGC Flight Guidance Computer FMEA Failure Modes and Effects AnalysisFLH Flight Level Hold FMS Flight Management SystemFL Flight (s) FOD Foreign Object DamageFNC Functional Check FPI Fluorescent Penetrant InspectionFP Flight Plan FS Fuselage StationFR Fluid Resistant (primer) FSDO Flight Standards District OfficeFSA Fleet Sample Aircraft FT Functional Test (same as FC)FSP Fatigue Sampling Program FWD ForwardFTP Functional Test Procedure FWS Flight Warning SystemFAA Federal Aviation Administration

GGA Go Around GE General ElectricGCU Generator Control Unit GLC Generator Line ContactorGMAP Ground Map GMM General Maintenance ManualGND Ground GPS Global Positioning SystemGPWS Ground Proximity Warning System GSE Gnd Support EquipmentGS Glideslope GVI General Visual Inspection




HHDG Heading HOT High Oil TemperatureHS Horizontal Stabilizer HF High FrequencyHMV Heavy Maintenance Visit HP High PressureHSD Hamilton Standard HSI Horizontal Situation IndicatorHSTCU Horizontal Stabilizer Trim Control Unit

IIAC Integrated Avionic Computer ICC IAPS Card CageIAS Indicated Airspeed IDFGS Intergrated Digital Flight Guidance SystemICU Integrated Comm Unit ILS Instrument Landing SystemIDG Integrated Drive Generator IRS Inertial Reference SystemIAPS Integrated Avionics Processor System ISC Industry Steering CommitteeINSP/VIS Inspection/Visual Check ISDU Inertial System Display UnitI/P InputIAPS Integrated Avionics Processor System ITT Inter Turbine Temperature

JJAA Joint Airworthiness Authorities JAR Joint Airworthiness RequirementJEMTOSS Jet Engine Maintenance Task Oriented Support System

LLC Line Check LCU Load Control ValveLDU Lamp Driven Unit LIRU Laser Inertial Reference System UnitLL Loft Line LNAV Laser NavigationLOC Localizer LOP Low Oil PressureLP Low Pressure LRN Long Range NavigationLRU Line Replaceable Unit LVDT Linear Variable Differential TransducerLUB Lubrication

MMAC Mean Aerodynamic Chord MB Messier BugattiMCP Multifunction Control Panel MDC Maint Diagnostics ComputerMEL Minimum Equipment List MMEL Master Minimum Equipment ListMFD Multifunction Display MFG ManufacturerMFS Multifunction Spoilers MFG REC Manufacturers RecommendationMLS Microwave Landing System MLG Main Landing GearMO Calendar Month(s) MM Maintenance ManualMP Magnetic Particle MOS Calendar Month(s)MPDH Maintenance Program Development Handbook MPD Maintenance Program Document

MPM Maintenance Planning Manual1 Examine context of usage to determine which term is applicable



M (cont’d)MPP Maintenance Program Proposal MPS Materials and Process SpecificationMRB Maintenance Review Board MRBR Maintenance Review Board ReportMRC Master Record Card MRM Maintenance Requirement ManualMSC Maintenance Steering Committee MSG-1 Maintenance Steering Group - 1st task forceMSG-2 Maintenance Steering Group - 2nd task force MSG-3 Maintenance Steering Group - 3rd task forceMSI Maintenance Significant Item MTBF Mean Time Between FailureMTLM Maintenance Time Limits Manual MTBUR Mean Time Between Unsched RemovalMTS Mach Trim System MWG Maintenance Working Group

NNACA National Advisory Committee on Aerodynamics N/A Not ApplicableNAV Navigation ND Navigation DisplayNDI Non Destructive Inspection NDT Non Destructive TestNLG Nose Landing Gear NR National RequirementNDTM Non Destructive Testing Manual NWS Nose Wheel Steering

OOAMP On Aircraft Maintenance Planning OI Opportunity InspectionOP Operational Check OPC Operational Check

PPBA Push Button Annunciator PCU Power Control UnitPDU Power Drive Unit PFD Primary Flight DisplayPLA Power Lever Angle POS PositionPMI Principal Maintenance Inspector PPH Policy and Procedures HandbookPRP Preparation PSE Principal Structural ElementPSI Pounds Per Square Inch PSEU Proximity Switch Electronic UnitPSU Passenger Service Unit PW Pratt & Whitney

QQA Quality Assurance QC Quality ControlQE Quality Engineering QAD Quick Attach DetachQEC Quick Engine Change QTY Quantity




RR/T Receiver/Transmitter RA1 Resolution Advisory

R&M Reliability and Maintainability RA1 Radio Altitude/Altimeter

RC Routine Check REO Repair Engineering Order (Bombardier)REU Remote Electronic Unit RF Radio FrequencyRFS Request for Service RII Required Inspection ItemRMI Radio Magnetic Indicator RLY RelayRS Restoration Task RMU Radio Management UnitRTA Receiver Transmitter Antenna RPM Revolutions Per MinuteRTU Radio Tuning Unit RST RestorationRVDT Rotary Variable Differential Transducer RTCA Radio Technical Commission for Aeronautics

SSAA Sulphuric Acid Anodizing SAT Static Air TemperatureSB Service Bulletin SCI Serial Control InterfaceSC Service Check SDI Special Detailed Inspection

SF Sample FleetSECU Spoiler Electronic Control Unit SI Sample InspectionSFA Sample Fleet Aircraft SIP Structural Inspection ProgramSID Supplemental Inspection Document SOV Shut-Off ValveSRN Short Range Navigation SRM Structural Repair ManualSPS Stall Protection System SSP Specific Sample PlanSSI Structural Significant Item STBY StandbySTA Station SVO ServoSV Service Task SWG Structural Working Group

TT Topcoat T/R Thrust ReverserTA Traffic Advisory TAS True Air SpeedTAT Total Air Temperature TBD To Be DeterminedTBO Time Between Overhaul TC Tire ChangeTCA Transport Canada Aviation TCAS Traffic Alert and Collision Avoid SystemTCS Touch Control Steering TI Threshold InspectionTII Threshold Inspection Interval TT Tap TestTOGA Takeoff Go Around TTG Time to GoTSO Technical Standard Orders TRU Transformer Rectifier Unit

UULB Underwater Locator Beacon ULD Underwater Locater DeviceUT Ultrasonic Test US Unserviceable




VVC Visual Check

VCK Visual Check VDC Volts DCVG Vertical Gyro VG Variable GeometryVHF Very High Frequency VIA Versatile Integrated AvionicsVNAV Vertical Navigation VOR VHF/Omnidirectional RangeVPTH Vertical Path VSI Vertical Speed IndVS Vertical Stabilizer

WWCF Whichever Comes First WDS Windshear Detection SystemWG Working Group WIG Whichever is greater WL Water Line WOW Weight on WheelsWPT Waypoint WS Wing StationWSS Windshear System WY WeeklyWXP Weather Radar Control Panel WX Weather Radar

XXR X-Ray

YYDS Yaw Damper System YRS Years

ZZIP Zonal Inspection Program




Program Overview

Systems/Powerplant ProgramEach System and Powerplant Inspection includes various inspection tasks including Detailed Inspections, Operational Checks, Functional Checks/Tests etc. They areperformed to ensure the inherent safety and reliability levels of the equipment. They also ensure that the safety and reliability of items is restored to their inherent levelswhen deterioration has occurred. In addition, the information necessary for design improvement of those items whose inherent reliability proves inadequate can beobtained. These tasks are designed to accomplish these goals at a minimum total cost, including maintenance costs and the costs of residual failure.

Zonal Inspection ProgramEach Zonal Inspection includes a General Visual Inspection (GVI) in order to determine the general condition and security of items contained in the Zonal InspectionProgram. Whenever physically possible, the Zonal Inspection will be conducted within touching distance unless otherwise stated. This includes checking for evidenceof degradation such as chafing of tubing, loose duct support, wiring damage, cable and pulley wear, fluid leaks, inadequate drainage, and for other conditions whichcould lead to corrosion/damage.

• The extent of a Zonal Inspection is defined by the access required and the instructions provided with the task.

• Doors and panels opened or removed during the Zonal Maintenance Program, and not having a separate defined zonal task, will receive a GVI.

• Zones which do not contain system or component installations and which receive adequate inspection from the structural programs are not assigned a zonaltask.

Structural Inspection ProgramUnder MSG-3 guidelines, each structural item is assessed in terms of its significance to continuing airworthiness, its susceptibility to deterioration processes (i.e. fatiguedamage, accidental damage and environmental deterioration) and the degree of difficulty in detecting such damage. A scheduled structural maintenance program hasbeen determined which will ensure continued airworthiness by providing a means to demonstrate that catastrophic failure due to the deterioration process will be avoidedthroughout the operational life of the Canadair CL600-2B19 series aircraft. Structural inspections are developed as part of the Maintenance Review Board Report(MRBR) process and aircraft type certification requirement. Requirements for detecting Accidental Damage (AD), Environmental Deterioration (ED) and FatigueDamage (FD) form the basis for the Canadair CL600-2B19 Structural Maintenance Program. Inspections performed to meet these criteria include Detailed VisualInspections (DVI) and Special Detailed Inspections (SDI), Non-Destructive Tests (NDT) are performed as a part of the SDI process.

All protective material (e.g., Corrosion Inhibiting Compounds, Paints, etc.) shall be re-applied, if removed, to perform the inspection/maintenance task. Areas exhibitingdeterioration of protective material or requiring application of this material shall be noted and applied.



Structural Significant Items (SSI)

Structures are divided into (2) categories based on the consequence of failure to aircraft safety.

• Structural Significant Item (SSI) is any detail, element or assembly which contributes significantly to carrying flight, ground, pressure or control loads andwhose failure could affect the structural integrity necessary for the safety of the aircraft.

• Secondary Structure is that which is judged not to be a Structural Significant Item. It is defined both externally and internally within zonal boundaries.

The assessment of SSI’s for selecting the type of maintenance task is based on the following:

The source of structural deterioration:

• Accidental Damage (AD)

• Environmental Deterioration (ED) / Corrosion

• Fatigue Damage (FD)

• The susceptibility of the structure to each source of deterioration.

• The consequence of structural deterioration to continuing airworthiness.

• The applicability and effectiveness of various methods of detecting structural deterioration, taking into account inspection thresholds and repeat intervals.

The assessment of SSI’s for AD, ED, and FD intervals in the MRBR may be shown in only one of the repeat interval columns, however, the task is intended toencompass any evidence of deterioration from Accidental, Environmental, and/or Fatigue damage. Intervals specified are displayed separately to show the primaryreason (driver) for the task/interval selected. Additionally, this adds the ability to verify that a corrosion program is an integral part of the Structural MaintenanceProgram ED tasks.

Structures Inspection Program Intervals

Critical portions of the airframe external and internal structure are visually inspected for signs of deterioration, thus confirming the continuation of structural integrity.When external inspections are specified for internally located structural items such as spars, spar caps, stringers, etc., the external structure immediately adjacent tothe identified internal items shall be visually examined externally for evidence of internal structural discrepancies. This external visual inspection can be accomplishedwithout removal of access doors or removal of other installed items. If there are external discrepancy indicators such as wrinkled skin, loose rivets, warping, fuel stains,buckling, oxidation etc., then a detailed internal inspection must be performed.

When inspection findings indicate the evidence of fatigue or corrosion deterioration, appropriate action shall be taken. Such action may include increased frequency ofinspections; a one-time inspection with repair action; an on-time modification of the item; application of corrosion preventive compounds, or other appropriate actiondepending on the consequences of allowing the deterioration to continue.

The Company will maintain a record for each aircraft showing the schedule of accomplishment and findings for the Structural Inspection Program and Zonal InspectionProgram. These records shall be available for ready reference by the assigned regulatory inspectors and for the purpose of establishing time interval changes to theMaintenance Program.



Program Outline

Line ChecksThe Line Checks consist of Inspection and Lubrication tasks performed at 3 and 10 calendar days. Job Cards are provided for these checks and the required items areaccounted for within this Time Limits Manual. Upon completion of the LC2 check, the authorized Inspector’s signature on the Aircraft Flight/Maintenance Log,Airworthiness Release Block, constitutes approval for return to service. This action is not required for the LC1 check. LC1 check is tracked by Mx Control.

“A” CheckThe “A” Check consists of several task type(s) to assure continued airworthiness of the Aircraft’s Powerplant, Systems, Components and Structures. It also consists ofa review of the Aircraft Flight/Maintenance Logbook and should be performed at stations where qualified maintenance personnel are available. The “A” Check shall beperformed within 500 FH. Upon completion of the “A” Check, the authorized Inspector’s signature on the Aircraft Flight/Maintenance Log, Airworthiness Release Block,constitutes approval for return to service.

NOTEEach Check is chained from one to the other and is considered a stand alone check. When one check is complete it is placed in an inactivestatus and the next sequence check becomes active. Example: CRJ A1 check is completed and placed into an inactive status, at this timeCRJ A2 becomes active. After completion of the CRJ A10 check the series begins anew with the CRJ A1 check. This is for the purpose oflevel-loading the A check program.

“C” Check C” Check is a comprehensive inspection of installations with maximum access to components and systems in various zones. In addition, qualitative and quantitativechecks are performed on the components / systems to detect deterioration in the performance of the components / systems. There are (5) “C” Check intervals: C, 2C,3C, 4C and 5C. Whenever a number precedes the letter, the interval for that task/inspection is the multiple of the “C” Check interval (5000 FH/FC which ever comesfirst (WCF)). For example, a 2C interval is to be accomplished at 10,000 FH/FC. Upon completion of the “C” Check, the authorized Inspector’s signature on the AircraftFlight/Maintenance Log, Airworthiness Release Block, constitutes approval for return to service.

Check IntervalLine Check 1 (LC1) 3 Calendar Days.Line Check 2 (LC2) 10 Calendar Days.

Check IntervalA Checks 1 through 10 500 FH/FC (and multiples)

Checks IntervalC Check 5,000 FH/FC WCF

2C Check 10,000 FH/FC WCF3C Check 15,000 FH/FC WCF



NOTEEach Check is compiled of tasks that are unique and repetitive for that interval. They are unchained and interval driven. “C” Check flight hour/flight cycle (FH/FC) and calendar intervals are “whichever comes first”.

Calendar CheckCalendar Checks are comprehensive inspections of installations with maximum access to components and systems in various zones. In addition, qualitative andquantitative checks are performed on the aircraft structure to detect deterioration. Calendar Checks, in some cases, are accomplished concurrently with a scheduledcheck. Upon completion of the “Calendar” Check, the authorized Inspector’s signature on the Aircraft Flight/Maintenance Log, Airworthiness Release Block, constitutesapproval for return to service when required following maintenance action.

NOTEEach Calendar Check is unique and repetitive. For example, a “48” Month Check is performed at 48 calendar month intervals. It does notcontain any elements of a “24” Month Check or a “48” Month Check, these checks must be performed in addition, if due. A 48 MO / 24 MOCalendar Check will be conducted at the intial threshold of 48 Months, all items on the 48 MO / 24 MO Check will be repeated at each 24Month interval. The repetitive 48 MO/ 24 MO Inspection Items may be conducted congruently with the 24 MO. Calendar Items less then 24MO are either packaged together in a Separately tracking item number or imbedded in the “A” Check program.

Computer Controlled TasksComputer Controlled Tasks require the scheduling of each component, item check and/or time changes in order to best utilize the maximum approved in-service timeof the item. The maintenance scheduling of such items is by unit, part number, serial number, aircraft number, location on aircraft and time remaining in service.

4C Check 20,000 FH/FC WCF5C Check 25,000 FH/FC WCF

Calendar ChecksInterval

(Threshold/Repeat)24 Month Check 24 MO 48 Month Check 48 MO72 Month Check 72 MO

72/48 Month Check 72 MO/ 48 MO96/48 Month Check 96 MO/ 48 MO96/72 Month Check 96 MO/ 72 MO120 Month Check 120 MO



WeighingPeriodic aircraft re-weighing for establishment of empty weight and center of gravity is performed at 36 month calender intervals. Aircraft Weight and Balance ControlProcedures are described in Chautauqua Airlines General Maintenance Manual.

High Pressure Bottle Hydrostatic TestThere are no specific Federal Aviation Regulations (FAR) for prescribing airworthiness standards of pressure cylinders used in aircraft systems such as oxygen, fireextinguishers and emergency air cylinders that are part of life support systems. Recognizing the lack of test data necessary to consider cylinder aging, internal corrosion,external pressure changes, cycles and extreme temperature changes, the FAA has adopted in the interest of safety, the rules and regulations of the Department ofTransportation (DOT) and applicable manufacturer’s recommendations as acceptable methods for controlling the hydrostatic test and life limits of pressure cylinders.Accordingly, hydrostatic test, inspection and life limits will be accomplished as set forth in Title 49 (Transportation), Subtitle B (Other Regulations relating toTransportation), Subchapter C (Hazardous Materials Regulations), 180.205 (General Requirements for Re qualification of Cylinders), unless otherwise specified by themanufacturer.

Fuel System LimitationsThe main purpose of the Fuel Tank Assessment analysis is to ensure that the possible ignition sources in the fuel tanks would be identified and precluded by designchanges for maintenance actions. Corrective actions included changes to the existing design and the addition of new maintenance actions, identified as Fuel SystemLimitations tasks.

Escalation or De-escalation of Maintenance Time IntervalsThe time limits shown in the Maintenance Program may be escalated and/or de-escalated in accordance with the Canadair CL600-2B19 MRM as approved by the FAA.In addition, the Company may request approval to escalate/de-escalate the time limits of individual items / tasks based on operating experience of the Canadair CL600-2B19 aircraft, supplemented by data from the Company and as approved by the FAA.

Where a task interval is de-escalated, the task will be carried out within the new task repeat interval from the effective date of the Inspection Program revision. Howeverthe task must be completed prior to the pre-revision task accomplishment deadline. This guideline does not apply to Airworthiness Limitations.

New Task Introduction / Existing task revisionAny mandatory Phase-in or Bridging Program takes precedence over the following: When a new task is introduced to the Inspection Program, the task will be carriedout within the new task repeat interval from the effective date of the Inspection Program revision approval. When a task has a threshold and a given aircraft has yet toreach the threshold time, for that aircraft the first inspection will be performed at the threshold listed in the Inspection Program. This guideline does not apply toAirworthiness Limitations. Where a task interval is revised from a given value to a lower value, the task should be done at the next convenient point, butwithin the new task repeat interval from the date of Inspection Program revision approval; the exception is if this rescheduling were to postpone the taskbeyond the pre-revision task accomplishment deadline.



Maintenance Short Term Escalation PolicyMaintenance intervals specified are not to be exceeded unless approved in accordance with the Short Term Escalation policy contained in the Chautauqua AirlinesGeneral Maintenance Manual.

Unscheduled EventsThere are occasions which may arise during operations of the aircraft where special Unscheduled Maintenance Checks will be required dependent on specificcircumstances. The range of Unscheduled Maintenance Checks are intended to cover events which may normally be expected (Example - Hard Landing Inspection).However, when other circumstances not covered are encountered, consult with the manufacturer or other appropriate sources. If an inspection is required, it must beperformed prior to further flight, unless a Special Flight Permit is issued to position the aircraft to a maintenance base where an in depth inspection can be made (Referto Chautauqua Airlines General Maintenance Manual).

Maintenance Time Limits Manual FormatThe MTLM is presented in the following tabbed sections: Systems/Powerplant, Structural, Zonal, AWL, FSL, CPCP, Other Required Maintenance Tasks, Appendix.

APPENDIXThe appendix of this manual may be amended and/or revised at the discretion of Chautauqua Airlines at any time as appropriate, and does not require FAA approvalprior to revision. The Appendix Section is considered as accepted by the FAA, and contains the following sections:

• 1. OTHER MAINTENANCE ITEMS

This part is for any non-required maintenance items that Chautauqua Airlines will perform, including Bombardier recommended tasks, Chautauqua Airlinesimplemented tasks, or other manufacturer's recommended tasks. The inspection package for task compliance is shown.

• 2. DELETED/PRECLUDED MAINTENANCE REQUIREMENTS

This part consists of tasks that have been deleted/precluded in the MRR or Chautauqua Airlines program due to new tasks that enhance or improve upon thedeleted task, task renumbering to achieve better conformity to existing numbering conventions, and similar.

• 3. TASK CROSS REFERENCE LIST

This is a list of tasks sorted in ascending order based on the task number, and shows the associated check package, task description, RPA Misc Task numberwhere appropriate, job card number.



Miscellaneous Program Information

Program RevisionsRevisions to the Chautauqua Airlines Inspection Program will be initiated by Chautauqua Airlines, based on the related Technical Documentation (MRM, MPD,Airworthiness Directives, Inspection Service Bulletins, etc.), as specified in Chautauqua Airlines General Maintenance Manual.

Accomplishment of items/tasks identified as necessary for incorporation into the Inspection Program will be initially tracked through company issued Engineering Orders(E.O.) or Fleet Campaign Directives (FCD) until such time that the additional item/task can be identified to Bombardier and incorporated as a revision to the Program.

Revisions are raised to reflect the embodiment of mandatory and non-mandatory modifications, inspections, and/or maintenance tasks, manufacturer’srecommendations or requirements, and the results of operational experience. Revision bars are located left and adjacent to the affected text.

The Inspection Program will be revised periodically to maintain or improve its effectiveness in light of findings and analyses conducted as part of the Continuous Analysisand Surveillance System as defined in Chautauqua Airlines General Maintenance Manual.

Revisions to the Canadair CL600-2B19 Maintenance Requirements Manual (MRM), and Maintenance Planning Document (MPD) document will be reviewed, and whereappropriate, changes will be incorporated in this Maintenance Program.

Revisions to the Inspection Program are allocated consecutive revision numbers.

Revisions to the Inspection Program Time Limitations must be approved by the Certificate Holding District Office (CHDO) and shall not be incorporated into theCompany’s Maintenance Program prior to CHDO approval.

Program Temporary Revisions

Temporary Revisions contain a Temporary Revision Record Page which is yellow in color. Temporary revisions are handled in the same manner as regularrevisions, except the revision information is recorded on the yellow Temporary Revision Record, instead of the white Revision Record [14 CFR121.135(a)(2) and (3)], and must be updated by the manual holder. CD-ROM versions of this manual will have the Temporary Revision inserted, theTemporary Revision Record page updated, and a list of all active Temporary Revisions will be printed on the CD.

Program Review and AuditThe data contained in this Program is reviewed and analyzed on a continuous basis as described in the CASS Program and methodology contained herein. Wheneverthe MTLM is revised, approved by the CHDO, and the necessary changes are implemented into the computerized record control system, each change will be reviewedby the Manager of Technical Services and audited by the Chautauqua Airlines QA auditing department to ensure all transactions have been posted or processedcorrectly and are tracking accurately against the effective aircraft, engines, and/or components as appropriate. This will be an on going process to ensure completeintergrity of the tracking and controls established for all maintenance and inspection tasks.



Intentionally Left Blank

.

Chapter 2Systems/Powerplant Program

Page iRevision 1 / April 15, 2008 CRJ200

Systems/Powerplant Program

IntroductionThe section following contains the various maintenance and inspection tasks that encompass the system/powerplant tasks. These tasks include such functions asDetailed Inspections (DVI/DI), Operational Checks (OPC), Functional Checks/Tests (FNC), etc. They are performed to ensure the inherent safety and reliability levelsof the equipment. They also ensure that the safety and reliability of items are restored to their inherent levels when deterioration has occurred.

Program NotesNOTE 1 Task interval based on manufacturer’s recommendation.

NOTE 2 Task interval in accordance with operator’s national regulation. When a task has two intervals, one being Note 2, the lower interval isrecommended. When a national regulation does not exist, the MRB Report Interval shall be followed.

NOTE 3 Task to be performed at brake/wheel/tire removal.

NOTE 4 Task to be performed at engine/APU change, as applicable, if not accomplished in the last 1000 FH.

NOTE 5 Task interval counted from component date of manufacture to expiration date.

NOTE 6 Task interval counted from date of last hydrostatic check of component.

NOTE 7 Note deleted Apr 21/06.

NOTE 8 Note deleted Dec 11/06.

NOTE 9 Ref. General Electric Engine Manual SEI 756, Airworthiness Limitations Section.

NOTE 10 This task is precluded by the Zonal Program task referenced in ZONAL REF. column.

NOTE 11 Note deleted Apr 30/96.

NOTE 12 The task is against optional equipment, and may not be installed on all aircraft.

NOTE 13 The manufacturer recommends that the operator perform one of the following maintenance programs for the APU:

• Hot Section Inspection in accordance with MRB Requirements

or

• Discard Program where compliance with manufacturers recommended rotating component discard limits is required. This discardprogram must be reviewed and approved by local Regulatory Authority and cannot be changed once selected, unless approved by localRegulatory Authority.

Chapter 2Systems/Powerplant Program

Page iiRevision 1 / April 15, 2008 CRJ200

NOTE 14 For these tasks, the task effectiveness should be monitored and the task interval adjusted, either up or down, to suit individual operators’environmental conditions and operating pattern.

NOTE 15 This task has a duplicate CMR requirement. Refer to Maintenance Requirements Manual, CSP A-053, PArt 2 Appendix A, for identificationof specific requirements regarding handling of Certification Maintenance Requirements (CMRs). Where the CMR interval for an MRB Reporttask is more restrictive, the CMR interval takes precedence. When the interval for an MRB Report task is more restrictive, the MRB Reporttask interval will take precedence.

NOTE 16 For task 32-00-00-05 only, the following phase in program is applicable to Nose Landing Gear (NLG) assemblies and Main Landing Gear(MLG) assemblies that will reach 120 months service life before reaching 20000 flight cycles service life.

For NLG and MLG assemblies that meet this condition, perform the restoration task 32-00-00-05 at the times specified below:

• For NLG and MLG assemblies with more that 120 months service life, do the restoration within 24 months from incorporation of the calendar limit into the operator’s approved maintenance program.

• For NLG and MLG assemblies with 96 months to 120 months service life, do the restoration within 36 months from incorporation of the calendar limit into the operator’s approved maintenance program.

• For NLG and MLG assemblies with less than 96 months service life, do the restoration on time at 120 months service life.

FormatThis manual section is presented in the following format:

• MRB Number - Indicates the control number from the MRM

• Task Description - Identifies the description of the component or maintenance requirement or zone

• Task - Indicates the type of maintenance task which must be accomplished

• Threshold - Indicates the maximum specified interval for the scheduled task of that item. Intervals are specified in flight hours unless indicated otherwise

• Repeat - Identifies the repeat interval for the scheduled task. Intervals are specified in flight hours unless indicated otherwise

• CMR/AD/LIFE - Identifies whether the task is a Certification Maintenance Requirement, Airworthiness Directive, or Life Limited Item

• Notes - Additional information such as modification status or aircraft model applicability of the task is included in this column as required.

Maintenance Time Limitations Manual CRJ200 Chapter 2: System/Powerplant

MRB No. Task Description Task Threshold Repeat ETOPS/CMR/AD Notes

21-24-30-03 Discard of the Cockpit Display Cooling Filter DS 1000 FH 1000 FH Note 14 (EFFECTIVITY: Post-Modsum TC601R12398 or Post SB 601R-21-019)

21-25-01-01 General Visual Inspection of the Class "C" Cargo Compartment Ducts and Clamps General Condition and Security

GVI10000 FH 10000 FH

Note 12

21-31-10-01 Operational Check of the Cabin Pressure Control System OP 5000 FH 5000 FH

21-31-13-01 Operational Check of the Cabin Pressure Control System (BITE Check) OP 1000 FH 1000 FH 21-32-01-01 Discard of the Cabin Pressure Control System Primary Outflow Valve Air Filter DS 5000 FH 5000 FH

21-32-01-02 Clean the Cabin Pressure Control System Primary Outflow Valve RS 5000 FH 5000 FH 21-32-04-01 Clean the Cabin Pressure Control System Secondary Outflow Valve RS 5000 FH 5000 FH 21-51-00-01 Operational Check of the Air Conditioning Overpressure Shutdown Circuit OP 5000 FH 5000 FH 21-51-04-01 Restoration of the Precoolers by Cleaning RS 16000 FH 16000 FH Note 1421-51-13-01 Detailed Inspection of the Air Cycle Machine Oil Levels DI 400 FH 400 FH Note 1421-51-13-05 Discard of the Air Cycle Machine Oil DS 1200 FH 1200 FH Note 1421-51-13-09 Restoration of the Heat Exchangers (Core) RS 8000 FH 8000 FH Note 1421-51-16-01 Clean the Coalescers on the Water Separators RS 1500 FH 1500 FH 21-51-16-03 Operational Check of the Air Cycle Machine Water Seperator Overboard Drains OP 2000 FH 2000 FH Post SB 601R-21-026 or Modsum TC601R13968

21-51-21-07 Detailed Inspection of the Bulkhead Check Valves DI 4000 FH 4000 FH Effectivity: P/N 92E20-3, -421-51-21-09 Detailed Inspection of the Bulkhead Check Valves DI 10000 FH 10000 FH Effectivity: P/N AE74341Z21-52-10-01 Operational Check of the Ram Air Shutoff Valve OP 5000 FH 5000 FH 21-55-07-01 Operational Check of the Cargo Fan Shutoff Valve OP 5000 FH 5000 FH Note 1221-55-07-03 Operational Check of the Conditioned Air Shutoff Valve OP 5000 FH 5000 FH Note 1221-55-07-05 Operational Check of the Cargo Exhaust Shutoff Valve OP 5000 FH 5000 FH Note 1222-11-00-03 Functional Check of the Servo Mount Slip Clutch Torque Setting FC 10000 FH 10000 FH 22-11-00-09 Lubrication of the Autopilot Servo and Servo Mount Engage Clutch Faces LU 6500 FH 6500 FH 23-31-13-01 Functional Check of the following: (1) Cabin Speaker System (Cabin and toilet),

(2) Automatic Volume Increase, (3) Passenger Address Over-Ride FunctionFC

5000 FH 5000 FH

23-51-00-03 Operational Check of the Pilot's Oxygen Mask Microphone OP 5000 FH 5000 FH 23-51-00-05 Operational Check of the Co-Pilots Oxygen Mask Microphone OP 5000 FH 5000 FH 23-51-00-07 Operational Check of the Observer's Oxygen Mask Microphone OP 5000 FH 5000 FH 23-51-01-03 Operational Check of the Audio Control Panel RT and EMER/NORMAL

SwitchesOP 10000 FH 10000 FH

23-61-00-01 Bonding and Megohmmeter Check of the Static Dischargers FC 5000 FH 5000 FH 23-71-01-01 Functional Check of the Cockpit Voice Recorder Intelligibility FC 36 MO 36 MO 23-71-03-01 Functional Check of the Cockpit Voice Recorder Underwater Locator Device FC 24 MO 24 MO P/N DK100

23-71-03-03 Restore the Cockpit Voice Recorder Underwater Locator Device RS 72 MO 72 MO Note 1, 523-82-01-01 Operational Check of the Standby NAV/COM Controller (CTL-23) OP 10000 FH 10000 FH 24-12-00-01 Visual Check of the IDG Oil Filter Differential Pressure Indicators VC 500 FH 500 FH 24-12-00-02 Service the IDG oil SV 500 FH 500 FH 24-12-00-03 Discard of the IDG Oil and the IDG Charge and Scavenge Oil Filter DS 1000 FH 1000 FH 24-12-00-05 Functional Check of the IDG Disconnect System (with Engines Running) FC 5000 FH 5000 FH 24-20-00-01 Functional Check of the AC Power Transfer Circuit FC 5000 FH 5000 FH 24-23-11-01 Operational Check of the Air Driven Generator System and Manual Deployment OP 4000 FH 4000 FH

24-23-11-03 Operational Check of the Air Driven Generator Electrical Distribution System OP 4000 FH 4000 FH

Revision 1 / April 15, 2008 Chapter 2: System/Powerplant 1 of 14



24-23-11-05 Discard of the ADG Uplock Mechanism Cartridges DS 42 MO Installed / 60 MO Life

42 MO Installed / 60 MO Life

Notes 2, 5 Task not required if cartridge not installed (dry ADG installation)

24-23-11-07 Lubrication of the ADG Pivot Shaft LU 4000 FH 4000 FH 24-30-00-01 Operational Check to Verify Individual Essential TRU Feed to the DC ESS BUS

and Battery BUSOP 5000 FH 5000 FH

24-30-00-03 Functional Check of the DC Power Distribution FC1000 FH 1000 FH

24-30-00-05 Operational Check of the DC Power Transfer Circuit OP 5000 FH 5000 FH 24-30-00-07 Operational Check of the Battery Circuitry OP 5000 FH 5000 FH 24-30-00-09 Operational Check of the TRU Fans OP 5000 FH 5000 FH 24-32-01-01 Functional Check of the Aircraft Main Battery FC 1500 FH 1500 FH 24-32-01-03 Restoration of the Aircraft Main Battery RS 12 MO 12 MO Note 124-32-03-01 Functional Check of the APU Battery FC 500 FH 500 FH 24-32-03-03 Restoration of the APU Battery RS 12 MO 12 MO Note 124-32-07-01 Operational Check of the Main and APU Battery Bus Solid State Controllers OP 12 MO 12 MO

25-11-01-03 Detailed Inspection of the Flight Compartment Seats DI 5000 FH 5000 FH 25-11-01-05 Detailed Inspection of the Flight Compartment Seat Belts and Harnesses DI 5000 FH 5000 FH 25-11-01-07 Operational Check of the Flight Compartment Seat Harness Inertia Reels OP 5000 FH 5000 FH 25-17-01-01 Functional Check of the Fortified Flight Compartment Door Decompression

LatchFC 5000 FH 5000 FH Note 12, Note 15 - C25-17-152-01

25-17-01-02 Functional Check of the Fortified Flight Compartment Door Decompression Latch

DI 1000 FH 1000 FH Note 12

25-17-01-03 Operational Check of the Fortified Flight Compartment Door Quick Release Hinges

OP 5000 FH 5000 FH Note 12

25-21-01-01 Functional Check of the Passenger Seats Break-Over Mechanism (last row only)

FC 5000 FH 5000 FH

25-21-01-03 Detailed Inspection of the Passenger Seat Locks and Seat Structure DI 5000 FH 5000 FH 25-21-02-01 Detailed Inspection of the Passenger Seat Belts DI 5000 FH 5000 FH 25-22-01-01 Detailed Inspection of the Flight Attendant Seats and Seat Structure DI 5000 FH 5000 FH 25-22-01-03 Detailed Inspection of the Flight Attendant Seat Attachment Points DI 5000 FH 5000 FH 25-22-02-01 Detailed Inspection of the Flight Attendant Seat Harness/Seat Belt Locking

MechanismDI 5000 FH 5000 FH

25-40-00-01 Detailed Inspection of the Lavatory Waste Compartment, Waste Compartment Door, Panel Surrounding the Waste Compartment Door and Sealant

DI2000 FH 2000 FH

Note 2

25-61-01-01 Functional Check of the Life Vests FC 24 MO 24 MO Note: Tracked by inspection sticker affixed to unit. This task is not effective to P/N: P01202-201

25-61-01-01-A GVI Life Vest GVI 60 MO Effectivity: P/N: P01202-20125-61-01-01-B RST Life Vest RST 120 MO 60 MO Effectivity: P/N: P01202-20125-61-02-01 Operational Check of the Flashlights OP 30 DY 30 DY 25-61-03-01 Detailed Inspection of the First Aid kit and Emergency Medical Kit for Condition

of SealsDI 30 DY 30 DY

25-61-04-01 General Visual Inspection of the Crash Axe for Security of Installation GVI 12 MO 12 MO 25-62-01-01 Discard of the Emergency Locator Transmitter Battery DS 24 MO 24 MO LIFE 25-62-01-03 Operational Check of the Emergency Locator Transmitter OP 12 MO 12 MO 25-63-01-01 Detailed Inspection of the Escape Rope and Safety Lines for General Condition

and SecurityDI 12 MO 12 MO




26-11-00-02 General Visual Inspection of the Jetpipe Sensing Loop Connectors and Wiring GVI 500 FH 500 FH

26-14-00-01 General Visual Inspection of the Main Landing Gear (MLG) Bay Overheat Detection System

GVI 5000 FH 5000 FH

26-14-01-01 Functional Check of the Main Landing Gear (MLG) Bay Detector Loops by Disconnecting the Connectors

FC 16000 FH 16000 FH

26-15-00-01 Restoration (Cleaning) of the Cargo Compartment Smoke Detectors RS 2500 FH 2500 FH 26-16-00-01 Operational Check of the Lavatory Smoke Detector (Using Smoke Source) OP 12 MO 12 MO 26-21-01-03 Operational Check of the Engine Fire Extinguishing System Switch/Lights OP 100 FH 100 FH 26-21-04-01 Functional Check of the Firex PUSH TO DISCH Switchlights by Disconnecting

ConnectorsFC 25000 FH 25000 FH

26-21-07-01 Visual Check of the Engine Fire Extinguishing Bottle Pressure Gauge VC 1000 FH 1000 FH 26-21-07-06 Hydrostatic Test of the Engine Fire Extinguishing Bottle FC 60 MO 60 MO 26-21-10-01-1 Discard of the Engine Fire Extinguishing Cartridges DS 72 MO 72 MO Notes 1, 5... P/N 897776

26-21-10-01-2 Discard of the Engine Fire Extinguishing Cartridges DS 120 MO 120 MO LIFE Notes 1, 5...P/N 897776-01

26-21-16-03 Detailed Inspection of the Engine Firex Extinguishing System Lines for Conditionand Security

DI 10000 FH 10000 FH

26-22-00-01 Functional Check of the APU Fire Extinguishing System by Disconnecting the Connector

FC 16000 FH 16000 FH

26-22-00-02 Operational Check of the APU fire extinguishing system switch/lights OP 500 FH 500 FH Note 15 - C26-20-131-0326-22-00-03 Functional Check of the APU Fire Extinguishing Unattended Mode Electrical

SystemFC 20000 FH 20000 FH

26-22-07-01 Visual Check of the APU Fire Extinguishing Bottle Pressure Gauge VC 1000 FH 1000 FH 26-22-07-06 Hydrostatic Test of the APU Fire Extinguishing Bottle FC 60 MO 60 MO 26-22-10-01-1 Discard of the APU Fire Extinguishing Bottle Cartridges DS 72 MO 72 MO LIFE Notes 1, 5...P/N 897776

26-22-10-01-2 Discard of the APU Fire Extinguishing Bottle Cartridges DS 120 MO 120 MO LIFE Notes 1, 5...P/N 897776-01

26-22-13-01 Detailed Inspection of the APU Fire Extinguishing System Lines for Condition and Security

DI 10000 FH 10000 FH

26-23-00-05 Hydrostatic Check of the Portable Fire Extinguishing Bottles FC 144 MO 144 MO Note: Tracked by inspection sticker affixed to unit26-23-01-01 General Visual Inspection of the Automatic Lavatory Fire Extinguisher Bottle and

Mounting Brackets for Condition and SecurityGVI 12 MO 12 MO Note 1

26-23-01-03 Weight Check of the Portable Fire Extinguisher Bottles FC 12 MO 12 MO Note 126-23-01-07 Weight Check of the Lavatory Fire Extinguisher Bottle FC 60 MO 60 MO 26-25-00-02 Detailed Inspection of the Cargo Compartment Fire Extinguishing System Lines

for Condition and SecurityDI 10000 FH 10000 FH

26-25-00-04 Operational Check Cargo Compartment Firex System OP 5000 FH 5000 FH26-25-00-07 Functional Check of the Cargo Compartment Fire Extinguishing System by

Disconnectiong the ConnectorsFC 25000 FH 25000 FH

26-25-01-01 Hydrostatic Check of the Cargo Compartment Firex Bottle FC 60 MO 60 MO 26-25-01-04 Visual Check of the Cargo Compartment Firex Bottle Pressure Gauge VC 2000 FH 2000 FH 26-25-01-07 Discard of the Cargo Compartment Firex Bottle Squibs DS 120 MO 120 MO Notes 1, 527-10-12-01 Operational Check of the Aileron Trim System OP 500 FH 500 FH 27-11-00-03 Detailed Inspection of the Aileron Mechanical Control Path in Pressurized Areas DI 10000 FH 10000 FH

27-11-00-05 Detailed Inspection of the Aileron and Aileron Autopilot Mechanical Control Path in Non Pressurized Areas

DI 5000 FH 5000 FH




27-11-00-07 Functional Check of the Aileron and Aileron Autopilot Control Cables for Correct Tension

FC 4000 FH 4000 FH

27-11-00-09 Functional Check (backlash) of the Aileron Control System FC 2000 FH 2000 FH 27-11-00-11 Operational Check of each Aileron PCU OP 500 FH 500 FH 27-11-15-01 Functional Check of the Aileron Breakout Bungee and Breakout Switch FC 8000 FH 8000 FH 27-13-01-01 Operational Check of the Aileron Disconnect System OP 500 FH 500 FH 27-15-01-01 Detailed Inspection of the Aileron Panel, PCU Attachment Points, Rub Seals

and Skin Surfaces for Condition and SecurityDI 5000 FH 5000 FH

27-15-05-01 Detailed Inspection of the aileron flutter dampers for fluid level, condition and security

DI 5000 FH 5000 FH Note 15 - C27-10-105-07

27-15-05-03 Functional Check of the Aileron Flutter Dampers FC 8000 FH 8000 FH 27-15-05-05 Operational Check of the aileron flutter fluid level transmitter switch OP 5000 FH 5000 FH Note 15 - C27-10-105-0727-20-00-03 Functional Check (backlash) of the rudder control system FC 5000 FH 5000 FH Note 15 - C27-10-105-0527-20-00-05 Detailed Inspection of the Rudder System Mechanical Control Path Elements,

such as Cables for Wear, Broken Strands, Corrosion, and Bird Caging. Check End Fittings, Turnbuckles, Pulleys, Rods, and Quadrants for Condition and Security

DI

10000 FH 10000 FH

27-20-00-07 Functional Check of the Rudder Control Cable for Correct Tension FC 4000 FH 4000 FH 27-20-00-10 Operational Check of the Rudder Trim System OP 500 FH 500 FH 27-20-00-13 Operational Check of the Each Rudder PCU OP 500 FH 500 FH 27-24-05-01 Detailed Inspection of the Rudder Panel Assembly and PCU Attachment Points,

Position Transmitters, Rub Seals and Skin for Condition and SecurityDI

5000 FH 5000 FH

27-31-00-03 Functional Check (backlash) of the elevator control system FC 5000 FH 5000 FH Note 15 - C27-10-105-0527-31-00-05 Operational Check of Each Elevator PCU OP 500 FH 500 FH 27-31-35-01 Detailed Inspection of the Elevator System Mechanical Path Control Elements

such as Cables for Wear, Broken Strands, Corrosion, and Bird Caging. Check End Fittings, Turnbuckles, Pulleys, Push/Pull Rods, and Quadrants for Condition and Security

DI

10000 FH 10000 FH

27-31-35-03 Functional Check of the Elevator and Elevator Autopilot Control System Cables for Correct Tesnion

FC 4000 FH 4000 FH

27-32-01-01 Functional Check of the Pitch Disconnect System FC 5000 FH 5000 FH 27-34-05-01 Detailed Inspection of the elevator flutter dampers for fluid level, condition and

securityDI 10000 FH 10000 FH Note 15 - C27-30-102-05

27-34-05-03 Operational Check of the elevator flutter damper fluid level transmitterswitch

OP 10000 FH 10000 FH Note 15 - C27-30-102-05

27-34-05-05 Functional Check of the Elevator Flutter Dampers FC 8000 FH 8000 FH 27-35-01-01 Detailed Inspection of the Angle-of-Attack (AOA) Vanes for Freedom of

MovementDI 100 FH 100 FH EFFECTIVITY: Pre-Modsum TC601R15984

27-35-01-07 Operational Check of the Stall Protection Computer by Pulling Circuit Breakers OP 10000 FH 10000 FH EFFECTIVITY: Pre-Modsum TC601R15984

27-40-01-05 Functional Check of the Horizontal Stabilizer Trim Actuator Assembly for Backlash

FC 10000 FH 10000 FH

27-40-01-07 Detailed Inspection of the Horizontal Stabilizer Trim Actuator Desiccant for Change of Color

DI 10000 FH 10000 FH

27-40-01-09 Functional Check of the Horizontal Stabilizer Trim System FC 5000 FH 5000 FH 27-40-01-11 Functional Check (Ground Maintenance Test) of the Horizontal Stabilizer Trim

Control UnitFC 5000 FH 5000 FH

27-40-01-14 Lubrication of the Horizontal Stabilizer Trim Actuator Screw Jack LU 5500 FH 5500 FH 27-40-01-17 Lubrication of the Horizontal Stab Hinge LU 10000 FH 10000 FH




27-50-01-01 Detailed Inspection of the following: 1) Flap Brake and Position Sensor Units 2) Flap BUTE Door Assemblies 3) Moveable Flap Vanes 4) Flap Panels 5) Flap Power Drive Units 6) Flap Position Transmitters 7) Flap Hinges

DI

2500 FH 2500 FH

27-50-01-03 Lubrication of the Flap System (Excluding Flap Actuators) LU 4000 FH 4000 FH 27-50-01-04 Lubrication of the Flap Actuators LU 500 FH 500 FH 27-50-01-05 Functional Check of the Flap System FC 5000 FH 5000 FH 27-50-01-07 Functional Check (ground maintenance test) of the FECU FC 5000 FH 5000 FH Note 15 - C27-50-111-0527-50-01-08 Detailed Inspection of the flap actuators DI 2500 FH 2500 FH Note 15 - C27-50-111-0727-50-01-09 Detailed Inspection of the Flap Flexible Drive Shafts DI 1500 FH 1500 FH 27-50-01-10 Detailed Inspection of the Flap Flexible Drive Shafts Core DI 5000 FH 5000 FH 27-51-00-01 Operational Check of the Skew Detection Unit (IBIT) OP 500 FH 500 FH EFFECTIVITY: Post-Modsum TC601R15480 or Post SB 601R-27-

11627-60-01-01 Functional Check of the Spoiler System including Maintenance Built in Test

(BITE)FC 5000 FH 5000 FH

27-60-01-03 Detailed Inspection of Condition and Security of the following: 1) Spoileron Panels, 2) Flight Spoiler Panels, 3) Ground Spoiler Panels

DI 5000 FH 5000 FH

27-60-01-05 Detailed Inspection for Condition, Security, and Leaks of the following: 1) Spoileron and Flight Spoiler Power Control Units, 2) Inboard Ground Spoiler Control Valve Manifold, 3) Outboard Ground Spoiler Control Valve Manifold, 4) Ground Spoiler Actuators

DI

5000 FH 5000 FH

27-60-01-07 Operational Check of the Manual Roll Priority Function OP 500 FH 500 FH 27-60-01-09 Operational Check of the Spoileron and Flight Spoiler Autostow Circuitry OP 5000 FH 5000 FH 27-60-01-11 Operational Check of the Spoiler System OP 5000 FH 5000 FH 27-60-01-15 Functional Check of the Spoiler Ground Lift Dump (GLD) FC 8000 FH 8000 FH 28-11-00-01 General Visual Inspection of the Fuel Access Panels and Fuel and Water Drain

Valves for Fuel LeaksGVI 3 DY 3 DY

28-11-00-02 Detailed Inspection of the Fuel Access Panels and Water Drain Valves and Fasteners, and their Surrounding Structure for Fuel Leakage

DI 60 MO 60 MO

28-11-00-05 Operational Check of the Water Drain Valves to Collect Water or Contaminants OP 3 DY 3 DY

28-11-00-07 Visual Check of the Fuel Filler Cap "O" Ring for Condition VC 60 MO 60 MO 28-12-00-01 Operational Check of the Main and Center Fuel Tank Pressure Relief Valves OP 3 DY 3 DY

28-12-00-03 Pressure Leak Testof the Fuel Tank Vent Shrouds and Fuel Line Shrouds and Fittings enclosed within the Pressurized Area

FC 60 MO 60 MO

28-21-00-03 Operational Check of the Both Engine Fuel Feed Shutoff Valves to verify if Both Valves are Operating in the "OPEN" and "CLOSED" Positions

OP 12 MO 12 MO

28-21-00-05 Functional Check of the Collector Tank Check Valve FC 60 MO 60 MO 28-24-00-03 Operational Check of the APU Fuel Feed Shutoff Valve to Physically verify if the

SOV goes to the "OPEN" and "CLOSED" Position by the Indicator on the Valve Housing

OP12 MO 12 MO

28-24-00-05 Restore the Fuel Transfer/ APU Pump Brushes RS 1800 AH / 1500 FH

1800 AH / 1500 FH

Effectivity: P/N’s 228078, 228077-2 and 228077-3

29-00-00-01 Hydraulic Fluid Analysis FC 5000 FH 5000 FH 29-11-00-03 Functional Check (Internal Leack Check) of the Hydraulic Systems #1 and# 2

Pressure Decay RateFC 5000 FH 5000 FH

29-11-05-01 Visual Check of the Hydraulic Systems #1 and #2 Pressure Filter Differential Pressure Indicators (Delta P)

VC 500 FH 500 FH




29-11-09-01 Discard of the Hydraulic Systems #1 and #2 Pressure Manifold Filter Elements DS 4000 FH 4000 FH

29-11-11-01 Visual Check of the Hydraulic Systems #1 and #2 Accumulators to verify Nitrogen Charge

VC 100 FH 100 FH

29-11-30-01 Discard of the Hydraulic Systems #1 and #2 Reservoir Mounted Check Valves DS 24000 FH 24000 FH

29-11-30-03 Discard of the Hydraulic Systems #1 and #2 Return Line Check Valves DS 24000 FH 24000 FH 29-11-36-01 Operational Check of the Hydraulic Systems #1 and #2 Firewall Shutoff Valves OP 5000 FH 5000 FH

29-11-38-01 Visual Check of the Hydraulic System #1 and #2 Case Drain Filter Differential Pressure Indicators (Delta P)

VC 500 FH 500 FH

29-11-40-01 Discard of the Hydraulic Systems #1 and #2 Case Drain Filter Elements DS 4000 FH 4000 FH 29-11-42-01 Detailed Inspection of the Hydraulic System Heat Exchanger Core for Foreign

Object DamageDI 5000 FH 5000 FH

29-11-44-01 Visual Check of the Hydraulic Systems #1 and #2 Return Manifold Differential Pressure Indicators (Delta P)

VC 500 FH 500 FH

29-11-46-01 Discard of the Hydraulic Systems #1 and #2 Return Manifold Filter Element DS 8000 FH 8000 FH 29-12-00-03 Functional Check (Internal Leak Check) of the Hydraulic System #3 Pressure

Decay RateFC 5000 FH 5000 FH

29-12-05-01 Visual Check of the Hydraulic System #3 Pressure Filter Differential Pressure Indicator (Delta P)

VC 500 FH 500 FH

29-12-09-01 Discard of the Hydraulic System #3 Pressure Manifold Element DS 4000 FH 4000 FH 29-12-11-01 Visual Check of the Hydraulic System #3 Accumulator to verify Nitrogen Charge VC 100 FH 100 FH

29-12-30-01 Discard of the Hydraulic System #3 Return Manifold Check Valve DS 24000 FH 24000 FH 29-12-30-03 Discard of the Hydraulic System #3 Return Manifold Return Fitting Check Valve DS 24000 FH 24000 FH

29-12-34-01 Visual Check of the Hydraulic System #3 Case Drain Filter Differential Pressure Indicators (Delta P)

VC 500 FH 500 FH

29-12-36-01 Discard of the Hydraulic System #3 Case Drain Filter Elements DS 4000 FH 4000 FH 29-12-36-03 Discard of the Hydraulic System #3 Return Manifold Filter Element DS 8000 FH 8000 FH 29-12-38-01 Visual Check of the Hydraulic System #3 Return Manifold Differential Pressure

IndicatorVC 500 FH 500 FH

30-12-00-01 Operational Check of the Wing Anti-Ice Standby Mode (Both Sides) OP 5000 FH 5000 FH 30-12-12-01 Functional Check of the wing anti−ice overheat sensors FC 4000 FH 4000 FH Note 15 - C30-10-141-0130-12-16-01 Operational Check of the Wing Anti-Ice Standby thermal Switches OP 5000 FH 5000 FH 30-12-23-01 Functional Check of the standby overheat switches FC 4000 FH 4000 FH Note 15 - C30-10-141-0131-31-03-01 Functional Check of the Flight Data Recorder (FDR) Underwater Locator Device FC 24 MO 24 MO

31-31-03-03 Restore the Flight Data Recorder (FDR) Underwater Locator Device RS 72 MO 72 MO Notes 1, 531-31-03-09 Functional Check of the Flight Data Recorder (FDR) Dedicated Sensors FC 15000 FH 15000 FH Post SB 601R-31-023 or Option CR 31-34031-41-00-01 Operational Check of the Aural Warning System 1 and 2 OP 5000 FH 5000 FH Aircraft with two Data Concentrator Units (DCU)31-41-00-03 Operational Check of the EICAS Reversionary Mode OP 5000 FH 5000 FH 31-41-04-01 Operational Check of DCU 1 OP 5000 FH 5000 FH Note 15 - C31-40-158-0131-41-04-03 Operational Check of DCU 2 OP 5000 FH 5000 FH Note 15 - C31-40-158-0131-41-04-04 Operational Check of the Data Concentrator Unit (DCU) 3 OP 4000 FH 4000 FH Note 1231-41-04-05 Operational Check of the Data Concentrator Unit (DCU) Fans OP 5000 FH 5000 FH 32-00-00-01 General Visual Inspection of the Main Landing Gear (MLG) and Nose Landing

Gear (NLG) Components and Doors for Condition and SecurityGVI 500 FH 500 FH




32-00-00-03 Lubricate the Fittings, Hinges, and Linkages on Main Landing Gear (MLG) and Nose Landing Gear (NLG). Clean and Lubricate Exposed (Chrome) Portion of Main and Nose Landing Gear Shock Struts

LU500 FH 500 FH

32-00-00-04 Lubrication of the Trailing Arm and Upper and Lower Shock Strut Joints on the Main Landing Gear (MLG)

LU 100 FH 100 FH

32-00-00-05-1 Restore the Main Landing Gear (MLG) Main Fitting RS 20000 FC / 120 MO

20000 FC / 120 MO

32-00-00-05-10 Restore the Main Landing Gear (MLG) and Nose Landing Gear (NLG) Gear Uplocks

RS 20000 FC / 120 MO

20000 FC / 120 MO

32-00-00-05-2 Restore the Main Landing Gear (MLG) Trailing Arm RS 20000 FC / 120 MO

20000 FC / 120 MO

32-00-00-05-3 Restore the Main Landing Gear (MLG) Down Lock/Sidestay Actuator RS 20000 FC / 120 MO

20000 FC / 120 MO

32-00-00-05-4 Restore the Main Landing Gear (MLG) and Nose Landing Gear (NLG) Axle RS 20000 FC / 120 MO

20000 FC / 120 MO

32-00-00-05-5 Restore the Main Landing Gear (MLG) Shock Strut RS 20000 FC / 120 MO

20000 FC / 120 MO

32-00-00-05-6 Restore the Nose Landing Gear (NLG) Downlock/Drag Brace RS 20000 FC / 120 MO

20000 FC / 120 MO

32-00-00-05-7 Restore the Nose Landing Gear (NLG) Shock Strut RS 20000 FC / 120 MO

20000 FC / 120 MO

32-00-00-05-8 Restore the Nose Landing Gear (NLG) Main Fitting RS 20000 FC / 120 MO

20000 FC / 120 MO

32-00-00-05-9 Restore the Nose Landing Gear (NLG) Actuator RS 20000 FC / 120 MO

20000 FC / 120 MO

32-00-00-07 Task Deleted Apr 21/06 32-00-00-09 Detailed Inspection of the Main Landing Gear (MLG) and Nose Landing Gear

(NLG) Shock Struts for Leakage, Condition, and SecurityDI 100 FH 100 FH

32-00-00-11 Functional Check of the Main Landing Gear (MLG) and Nose Landing Gear (NLG) Shock Struts for Correct Chrome Extension Length

FC 500 FH 500 FH

32-00-00-13 Lubricate the Threads of the Main Landing Gear (MLG) and Nose Landing Gear (NLG) Axles and Axle Nuts

LU Refer to Note Refer to Note Note 3

32-00-00-15 Detailed Inspection of the Main Landing Gear (MLG) and Nose Landing Gear (NLG) Axles for Corrosion and Damage

DI Refer to Note Refer to Note Note 3

32-00-00-17-1 Discard the Main Landing Gear (MLG) Main Fitting DS Refer to Note Refer to Note LIFE AWL's: 32-11-110a-h32-00-00-17-2 Discard the Main Landing Gear (MLG) Trailing Arm DS Refer to Note Refer to Note LIFE AWL's: 32-11-108a-d32-00-00-17-3 Discard the Main Landing Gear (MLG) Down Lock/Sidestay Actuator DS Refer to Note Refer to Note LIFE AWL's: 32-11-112, 32-11-113, 32-11-114, 32-11-11732-00-00-17-4 Discard the Main Landing Gear (MLG) and Nose Landing Gear (NLG) Axle DS Refer to Note Refer to Note LIFE AWL's: 32-11-111, 32-21-101a-k32-00-00-17-5 Discard the Main Landing Gear (MLG) Shock Strut DS Refer to Note Refer to Note LIFE AWL's: 32-11-106a-b32-00-00-17-6 Discard the Nose Landing Gear (NLG) Downlock/Drag Brace DS Refer to Note Refer to Note LIFE AWL's: 21-21-101a-k, 21-21-103, 32-21-104a-b




32-00-00-17-7 Discard the Nose Landing Gear (NLG) Shock Strut DS Refer to Note Refer to Note LIFE AWL's: 32-21-101a-k32-00-00-17-8 Discard the Nose Landing Gear (NLG) Main Fitting DS Refer to Note Refer to Note LIFE AWL's: 32-21-101a-k32-00-00-19 Detailed Inspection of the Main Landing Gear (MLG) and Nose Landing Gear

(NLG) Components for Leakage and SecurityDI 5000 FH 5000 FH

32-00-00-20 Detailed Inspection of the Main Landing Gear (MLG) and Nose Landing Gear (NLG) Doors for Leakage, Condition and Security

DI 4000 FH 4000 FH

32-00-00-21 Servicing of the Main Landing Gear (MLG) and Nose Landing Gear (NLG) Shock Struts

SV 2500 FH 2500 FH

32-34-00-01 Detailed Inspection of the Main Landing Gear (MLG) and Nose Landing Gear (NLG) Manual Release Control Mechanism and Components for Leakage, Wear, Broken Strands, Corrosion or Kinks. Check End Fitting Turnbuckle, Brackets, Fairleads and Quadrants for Wear,

DI

4000 FH 4000 FH

32-34-00-03 Functional Check of the Landing Gear Manual Release System FC 4000 FH 4000 FH 32-40-00-01 Visual Check of the Main Landing Gear (MLG) and Nose Landing Gear (NLG)

Wheel/Tire Assemblies for Damage and WearVC 3 DY 3 DY

32-40-00-03 Functional Check of the Main Landing Gear (MLG) and Nose Landing Gear (NLG) Wheel Assemblies for Inflation Pressure

FC 3 DY 3 DY

32-40-00-05 Visual Check of the Main Landing Gear (MLG) and Nose Landing Gear (NLG) Tires for Correct Tread Depth

VC 3 DY 3 DY

32-43-06-01 Functional Check of the Brake Accumulator Pressure and Service If Required FC 100 FH 100 FH

32-43-06-03 Functional Check of the Brake System Volumetric (Hydraulic) Fuses FC 5000 FH 5000 FH 32-43-06-05 Lubricate the Brake Control Valve LU 2500 FH 2500 FH 32-43-16-01 General Visual Inspection of the Brake System Hydraulic Lines and

Components for Condition, Security and LeaksGVI 100 FH 100 FH

32-43-21-01 Detailed Inspection of the Parking and Main Brake Control Mechanical Path for Security of Attachment and Fouling

DI 5000 FH 5000 FH

32-43-26-01 Detailed Inspection of the Brake Wear Pin Indicators DI 3 DY 3 DY 32-44-00-01 Functional Check of the (Built-In Test) Anti-Skid Control Unit (ASCU) FC 500 FH 500 FH 32-45-00-01 Lubrication of the Parking Brake Handle Shaft LU 1000 FH 1000 FH Triumph Control P/N 7-44856-9, -11, -13, -15, -1732-50-01-05 Detailed Inspection of the Nose Wheel Steering Actuator Assemblies for

Condition and SecurityDI 5000 FH 5000 FH

32-50-01-09 Lubrication of the Nose Wheel Steering Collar LU 500 FH 500 FH 32-60-01-01 Functional Check (BITE Test) of the Proximity Sensor Electronics Unit (PSEU) FC 500 FH 500 FH

33-42-00-01 General Visual Inspection of the Position Light Lenses for Crazing and Diffusion of Light Source

GVI 5000 FH 5000 FH

33-50-00-01 Operational Check of the Emergency Lighting System OP 500 FH 500 FH 33-50-00-03 Task Deleted Apr 21/06 33-50-00-05 General Visual Inspection Emergency Floor Path Lighting GVI See Note See Note EFFECTIVITY: Post−Modsum TC601R101452, Note 1, this task is

not effective to the CHQ fleet at this time.33-51-04-01 Restore the Emergency Lighting System Battery Packs RS 18 MO 18 MO P/N RPS1-B33-51-04-03 Operational Check (Self Test) of the Emergency Lighting System Battery Packs

1, 2, 3 and 4OP 5000 FH 5000 FH

33-51-04-05 Functional Check of the Door Handle BETA Lights to Check Luminosity FC 24 MO 24 MO 34-11-00-01 Detailed Inspection of the Main and Standby Pitot-Static Drains for Moisture DI 500 FH 500 FH

34-11-00-05 General Visual Inspection of the Main Pitot-Static and Standby Pitot Probes GVI 500 FH 500 FH 34-11-00-07 Functional Check (Leak Check) of the Main and Standby Pitot Static Systems FC 24 MO 24 MO




34-12-01-01 Restoration of the Standby Airspeed/ Altimeter Indicator (Calibration Check) RS 24 MO 24 MO Note 2 EFFECTIVITY: Pre-Modsum TC601R15984 or Pre-SB 601R-34-137

34-12-01-03 Functional Check of the Intergrated Standby Instument System (Altitude/Airspeed Scale Error Check)

FC 8000 FH 8000 FH EFFECTIVITY: Post-Modsum TC601R15984 or Post SB 601R-34-137

34-13-01-01 Functional Check of the Air Data Computer Overspeed Aural Warning FC 24 MO 24 MO 34-13-01-03 Functional Check of the Air Data Computer (Altitude/Airspeed Scale Error

Check)FC 10000 FH 10000 FH

34-22-01-01 Functional Check of the Standby Compass FC 36 MO 36 MO Note 234-25-11-01 Operational Check of the Display Reversionary Switch OP 5000 FH 5000 FH 34-32-07-01 Detailed Inspection of the Heads-Up Guidance Sys Drive Unit Fan Filter, and

clean if necessaryDI 5000 FH 5000 FH Note 12

34-45-00-01 Operational Check of the Inertial Reference System (ATT Mode) OP 5000 FH 5000 FH Note 1235-11-03-01 Hydrostatic Test of the Crew Oxygen Cylinder FC 36 MO 36 MO 35-11-03-03 Visual Check of EICAS and pressure gauges for agreement VC 500 FH 500 FH Note 15 - C35-10-128-0135-11-03-05 Discard of the Crew Oxygen Cylinder DS 180 MO 180 MO LIFE Notes 1, 535-11-05-01 Operational Check of the Crew Oxygen System OP 5000 FH 5000 FH 35-11-05-03 Detailed Inspection of the Crew Oxygen Masks DI 4000 FH 4000 FH 35-23-07-01 Operational Check of the Passenger Oxygen Manual Deploy System OP 24 MO 24 MO Note 135-23-07-03 Operational Check of the Passenger Oxygen System Automatic Deploy Mode OP 24 MO 24 MO Note 1

35-23-07-05 Detailed Inspection of the Passenger Oxygen Masks DI 36 MO 36 MO 35-23-13-03 Discard of the Oxygen Generator DS 144 MO 144 MO LIFE Notes 1, 535-23-13-05 Operational Check (Drop Test) of the of Cabin Masks OP 24 MO 24 MO 35-31-05-01 Hydrostatic Check of the Portable Oxygen Cylinder FC 60 MO 60 MO Note: Tracked by inspection sticker affixed to unit35-31-05-03 Operational Check of the Portable Oxygen Equipment OP 12 MO 12 MO 35-31-05-05 General Visual Inspection of the Portable Oxygen Cylinder Face Mask, Hose,

Mountings, Attachments, and Connectors for General ConditionGVI 12 MO 12 MO

35-31-07-03 Discard of the Portable Breathing Equipmentment (PBE) Unit DS 120 MO 120 MO LIFE Note: Tracked by inspection sticker affixed to unit36-11-10-01 Detailed Inspection of the APU Supply Check Valve DI 5000 FH 5000 FH 36-21-07-01 Operational Check of Each Thermal Switch in the Wing Leading Edges OP 24000 FH 24000 FH 38-11-01-01 Restore the Galley Water Tank Filter RS 12 MO 12 MO Note 14, Pre-EO3801238-11-01-07 Sanitization of the Potable Water System SV 12 MO 12 MO Note 238-21-01-01 Restore the Lavatory Water Tank Filter RS 12 MO 12 MO 'Note 14, Pre-EO3801238-30-01-01 Detailed Inspection of the toilet Drain Valve DI 24 MO 24 MO 38-30-01-03 Detailed Inspection of the toilet Waste Tank DI 24 MO 24 MO 49-11-00-01 Detailed Inspection of the APU Enclosure Assembly for Cracks and Sealant

Condition, and to verify Structural IntegrityDI 5000 FH 5000 FH

49-12-00-01 Detailed Inspection of the APU Mounting Skid Mounting Bolts, Support Bracket, and Link Support for Security, Installation and Condition, Paying Particular Attention to Welds

DI5000 FH 5000 FH

49-14-00-01 Detailed Inspection of the Exterior of the APU Air Intake Ducting for Cracks, Corrosion, Integrity and Security of Installation of Attaching Hardware

DI2000 FH 2000 FH

Note 14

49-14-00-03 Detailed Inspection of the APU Air Intake Assembly Desiccant for Evidence of Moisture

DI 5000 FH 5000 FH

49-14-19-01 Detailed Inspection of the APU Air Intake Assembly Door Mechanism for Cracks, Corrosion, Integrity and Security of Installation of attaching Hardware

DI15000 FH 15000 FH




49-15-00-01 Detailed Inspection of the APU Drain System Tubes and Hoses for Condition, Security of Installation, and Freedom from Obstruction

DI15000 FH / Note 4 15000 FH / Note 4

49-20-00-01 APU Hot Section Inspection (Restoration) Per Vendor Maintenance Manual RS 3500 AH 3500 AH Effective for APU's on HSI inspection program49-20-00-03 General Visual Inspection of the Externally Visible Portions of APU Inlet Duct

within the APU EnclosureGVI 2000 FH 2000 FH

49-20-00-17 General Visual Inspection of the APU Turbine Housing GVI 2000 FH 2000 FH 49-24-00-03 Detailed Inspection of the Magnetic Element In the APU Drain Plug DI 300 AH 300 AH 49-24-00-05 Detailed Inspection of the APU Oil Level DI 300 AH 300 AH 49-24-00-07 General Visual Inspection of the APU Gearbox Housing/ Mounting Boss for

External Leakage, Condition and SecurityGVI 2000 FH 2000 FH

49-24-00-11 Detailed Inspection of the APU Gearbox Vent Line for Signs of Oil Coking DI 1500 AH 1500 AH Pre Honeywell SB GTCP36-49-774949-26-00-01 General Visual Inspection of the Visible Portion of the APU Fan Discharge Duct,

Flexduct(s) and Inlet Duct for Security and ConditionGVI 2000 FH 2000 FH

49-31-00-01 General Visual Inspection of the APU Fuel System Components, Seals, Lines, and Interface Connections, within the APU Enclosure for Security of Installation, Leakage, or Chafing

GVI300 AH 300 AH

49-31-05-01 Visual Check of the APU Fuel Filter Delta P Indicator VC 300 AH 300 AH 49-31-05-03 Discard of the APU Fuel Filter Element DS 750 AH 750 AH 49-42-10-01 Detailed Inspection of the APU Igniter Plugs and Leads (Removed) for Security

and Evidence of Arching and Carbonization per Vendor Maintenance ManualDI

1200 AH 1200 AH

49-43-00-01 Operational Check of the APU Remote Switches to Verify Remote Shutdown OP 5000 FH 5000 FH

49-44-00-01 Detailed Inspection of the APU Starter Brush Wear per Vendor Maintenance Manual

DI 3000 AH 3000 AH

49-60-00-01 General Visual Inspection of the Visible Portion of APU Wiring Harness and Connectors within APU Enclosure for Damage, Security of Installation and Chafing

GVI3500 AH 3500 AH

49-81-00-01 Detailed Inspection of the APU Exhaust Installation for Security and Evidence of Cracks, Fragmentation, or Damage

DI 3000 FH 3000 FH

49-91-00-05 General Visual Inspection of the APU Oil System External Plumbing, Seals and Components for Leakage

GVI 2000 FH 2000 FH

49-91-07-01 Restoration of the APU Oil Cooler by Cleaning RS 3500 AH 3500 AH Note 1449-91-10-01 Visual Check of the APU Oil Filter Delta P Indicator VC 300 AH 300 AH 49-91-10-03 Discard of the APU Oil Filter Element DS 750 AH 750 AH 52-00-00-01-1 Lubrication of the Avionics Compartment Door LU 1000 FH 1000 FH 52-00-00-01-2 Lubrication of the Service/Emergency Door LU 1000 FH 1000 FH 52-00-00-01-3 Lubrication of the Cargo Compartment Door LU 1000 FH 1000 FH 52-00-00-01-4 Lubrication of the Rear Fuselage Equipment Compartment Door LU 1000 FH 1000 FH 52-00-00-02 Lubrication of the Passenger Door Lockpins LU 500 FH 500 FH Note: Task Cannot be escalated above 600 Flight Hours

EFFECTIVITY: Pre-Modsum TC601R1319352-00-00-03-1 Detailed Inspection of all Hinges, Lock Pins, Latches, Door Actuation Controls

(Internal and External) and Pressure Seals on the Crew Escape HatchDI

5000 FH 5000 FH

52-00-00-03-2 Detailed Inspection of all Hinges, Lock Pins, Latches, Door Actuation Controls (Internal and External) and Pressure Seals on the LH and RH Overwing Emergency Exits

DI5000 FH 5000 FH




52-00-00-03-3 Detailed Inspection of all Hinges, Lock Pins, Latches, Door Actuation Controls (Internal and External) and Pressure Seals on the Maintenance Access Panels

DI5000 FH 5000 FH

52-00-00-04 Lubrication of the Passenger Door Hinges, Latches, Door Actuation Controls (Internal and External), Vent Flaps, Tracks, Handrail Mechanisms, and for Aircraft Post SB 601R-52-090 or Modsum TC601R13909 , Lubricate the Aft Counterbalance Support-Pulley Bolt

LU

1000 FH 1000 FH

EFFECTIVITY: Pre-Modsum TC601R13193

52-00-00-05-1 Functional Check of the Passenger Door FC 2500 FH 2500 FH EFFECTIVITY: Pre-Modsum TC601R1319352-00-00-05-2 Functional Check of the Service / Emergency Door FC 2500 FH 2500 FH 52-00-00-06-1 Detailed Inspection of the Internal Components of the Passenger Door DI 5000 FH 5000 FH EFFECTIVITY: Pre-Modsum TC601R1319352-00-00-06-2 Detailed Inspection of the Internal Components of the Service / Emergency Door DI 5000 FH 5000 FH

52-00-00-07-1 Detailed Inspection of the Avionics Service Door for Condition and Security DI 2500 FH 2500 FH 52-00-00-07-2 Detailed Inspection of the LH Forward Equipment Compartment Door for

Condition and SecurityDI 2500 FH 2500 FH

52-00-00-07-3 Detailed Inspection of the RH Forward Equipment Compartment Door for Condition and Security

DI 2500 FH 2500 FH

52-00-00-07-4 Detailed Inspection of the Rear Fuselage Equipment Compartment Door for Condition and Security

DI 2500 FH 2500 FH

52-00-00-08 Detailed Inspection of the Cargo/Baggage Compartment Door for Condition and Security

DI 2000 FH 2000 FH

52-00-00-09-1 Lubrication of the Crew Escape Hatch LU 5000 FH 5000 FH 52-00-00-09-2 Lubrication of the Overwing Emergency Exit LU 5000 FH 5000 FH 52-00-00-09-3 Lubrication of the Maintenance Access Panels LU 5000 FH 5000 FH 52-00-00-11-1 Functional Check of the Crew Escape Hatch FC 5000 FH 5000 FH 52-00-00-11-2 Functional Check of the RH Overwing Emergency Door FC 5000 FH 5000 FH 52-00-00-11-3 Functional Check of the LH Overwing Emergency Door FC 5000 FH 5000 FH 52-00-00-17-1 Detailed Inspection of the External Portion of the Passenger Door DI 1000 FH 1000 FH EFFECTIVITY: Pre-Modsum TC601R1319352-00-00-17-2 Detailed Inspection of the External Portion of the Service/Emergency Door DI 1000 FH 1000 FH 52-00-00-18 Lubrication of the Passenger Door Outer Handle LU

500 FH 500 FH Note: Task Cannot be escalated above 600 Flight Hours

EFFECTIVITY: Pre-Modsum TC601R13193 and Pre-Modsum TC601R14500

52-00-00-19 Lubrication of the Passenger Door Outer Handle LU 2500 FH 2500 FH EFFECTIVITY: Pre-Modsum TC601R13193 and Post-Modsum TC601R14500

52-00-00-20 Detailed Inspection of the Crew Escape Hatch Mechanism (Internal and External)

DI 12 MO 12 MO

52-11-00-01 Detailed Inspection of the Passenger Door Support Wheel Cables and Pulleys DI 5000 FH 5000 FH EFFECTIVITY: Post-Modsum TC601R13193

52-11-00-02 Detailed Inspection of the Passenger Door Latch Mechanism DI 5000 FH 5000 FH EFFECTIVITY: Post-Modsum TC601R1319352-11-00-03 Lubrication of the Passenger Door Hinge LU 1000 FH 1000 FH EFFECTIVITY: Post-Modsum TC601R1319352-11-00-04 Functional Check of the Passenger Door FC 5000 FH 5000 FH EFFECTIVITY: Post-Modsum TC601R1319352-11-00-05 Lubrication of the Passenger Door Latch Pins and Latch Cam LU 500 FH 500 FH EFFECTIVITY: Post-Modsum TC601R1319352-11-00-06 Detailed Inspection of the Passenger Door Locking Devices DI 5000 FH 5000 FH EFFECTIVITY: Post-Modsum TC601R1319371-12-00-03 Detailed Inspection of the Core Cowl Pressure Relief Doors DI 5000 FH 5000 FH 71-16-00-03 Detailed Inspection of the A7 Attach Flange for Condition and Security of

InstallationDI 5000 FH 5000 FH

71-16-00-07 Detailed Inspection of the Engine Forward Core Cowl Assembly for Loose attenuating Panels and Loose or Missing Fasteners

DI 5000 FH 5000 FH

71-16-00-09 Detailed Inspection of the Engine Forward Core Cowl Assembly Sound Attenuating Panels for Delamination

DI 5000 FH 5000 FH




71-21-00-01 Detailed Inspection of the forward Engine Mount Assembly, Yoke Assembly and Link Assembly for Cracks, Corrosion, Integrity, and Security of Installation of attaching Hardware

DI Refer to Note Refer to Note

LIFE Note 4

71-22-00-01 Detailed Inspection of the Rear Engine Mount and Components for Cracks, Missing Hardware or Evidence of Damage and Corrosion

DI Refer to Note Refer to Note Note 4

71-31-00-01 General Visual Inspection of the Nacelle/ Pylon Firewall for Cracks, Damage, or Deterioration and Powerplant/Aircraft System Firewall Connections (Hydraulic, Fuel, Oil Lines, Etc) for Evidence of Leaks, Condition and Security of Installation

GVI

5000 FH 5000 FH

71-51-00-02 Detailed Inspection of the Powerplant Core Cowl Master Harness A (Red) DI Refer to Note Refer to Note Note 471-51-00-04 Detailed Inspection of the Powerplant Core Cowl Master Harness B (Violet) DI Refer to Note Refer to Note Note 471-52-00-02 Detailed Inspection of the Powerplant Nose Cowl Accessories Harness (orange) DI Refer to Note Refer to Note Note 4

71-61-00-01 General Visual Inspection of the Engine Nose Inlet Cowl Assembly for Condition and Security of Installation

GVI 2500 FH 2500 FH

71-61-00-05 General Visual Inspection of the Engine Nose Inlet Cowl Assembly Access Panel Fasteners and Support Brackets for Anti-Icing Equipment and the Power Drive Units, for Condition and Security of Installation

GVI5000 FH 5000 FH

71-61-00-07 Detailed Inspection Nacelle upper and lower nose cowl access panel fastners and grommets for security

DI 5000 FH 5000 FH

72-21-00-01 Discard the Engine Fan Disk DS Refer to Note Refer to Note LIFE Notes 1, 972-21-00-03 Detailed Inspection of the Engine Fan Blades for Evidence of FOD, Paying

Special Attention to the Blade Leading EdgesDI 500 FH 500 FH

72-21-00-05 General Visual Inspection of the Engine Fan Spinner and Attaching Hardware GVI 500 FH 500 FH

72-21-00-07 Discard the Engine Fan forward Shaft DS Refer to Note Refer to Note LIFE Notes 1, 972-21-00-09 Detailed Inspection of the Engine Master Chip Detector Indicator DI 100 FH 100 FH 72-22-00-01 Discard the Engine Fan Drive Shaft DS Refer to Note Refer to Note LIFE Notes 1, 972-23-00-01 Detailed Inspection of the Engine Fan Stator Forward Engine Mounts for Mount

Cracks or Distortion, Aft Fan Case for Cracks or Distortion, Security and Condition of Attaching Hardware, and Condition of Anti Corrosion Coating

DI

5000 FH 5000 FH

72-23-00-03 Detailed Inspection of the Exterior of the Engine Fan Case for Evidence of Cracks or Distortion, Mechanical Damage, and Corrosion

DI 5000 FH 5000 FH

72-23-00-07 General Visual Inspection of the Engine Fan Shroud Core Material for Condition,Security, Heavy Rubs and Damage

GVI 500 FH 500 FH

72-31-00-01 Detailed Inspection of the Engine Front Frame for Evidence of Cracking or Structural Deterioration

DI 5000 FH 5000 FH

72-32-00-01 Detailed Inspection of the Engine Variable Guide Vanes Actuating Assembly, Unison Rings, and Linkages

DI 5000 FH 5000 FH

72-32-00-03 Special Detailed Inspection of the Engine Variable Guide Vanes and Stationary Vanes for Rubs and Internal Damage Using Borescope, as Far as is Visible through Existing Ports

SDI5000 FH 5000 FH

72-32-00-05 Lubricate the Engine Variable Guide Vane Linkage Rod End Bearings LU 1000 FH 1000 FH 72-33-00-01 Special Detailed Inspection of the Engine Compressor Blades for Evidence of

FOD, Cracks, Rubs, and Tip Curl Using BorescopeSDI 5000 FH 5000 FH

72-33-00-03-1 Discard of the Engine Compressor Rotor Stage 1 Disc DS Refer to Note Refer to Note LIFE Notes 1, 972-33-00-03-2 Discard of the Engine Compressor Rotor Forward Shaft DS Refer to Note Refer to Note LIFE Notes 1, 972-33-00-03-3 Discard of the Engine Compressor Rotor Stage 2 Disc DS Refer to Note Refer to Note LIFE Notes 1, 972-33-00-03-4 Discard of the Engine Compressor Rotor Stage 3-8 Rotor Spool DS Refer to Note Refer to Note LIFE Notes 1, 9




72-33-00-03-5 Discard of the Engine Compressor Rotor Stage 10-14 Rotor Spool DS Refer to Note Refer to Note LIFE Notes 1, 972-33-00-03-6 Discard of the Engine Compressor Rotor Rear Shaft CDP Seal DS Refer to Note Refer to Note LIFE Notes 1, 972-33-00-03-7 Discard of the Engine Compressor Rotor Rear Shaft DS Refer to Note Refer to Note LIFE Notes 1, 972-33-00-03-8 Discard of the Engine Compressor Rotor Stage 9 Disc DS Refer to Note Refer to Note LIFE Notes 1, 972-41-00-03 General Visual Inspection of the Engine Combustor Overboard Drain for

Evidence of Oil LeakageGVI 500 FH 500 FH

72-42-00-01 Special Detailed Inspection of the Engine Combustor Liner using Borescope, to Detect Cracks, Fragmentation, Mechanical or Thermal Stress Related Damage

SDI3000 EH 3000 EH

72-42-00-03 Special Detailed Inspection of the Stage 1 Nozzle for Evidence of Burns, Cracks or Damage using Borescope

SDI 3000 EH 3000 EH

72-43-00-01 Detailed Inspection of the Engine Thermal Blanket for Condition and Security DI 500 FH 500 FH

72-44-00-01 Detailed Inspection of the Engine Rear Main Mount for Evidence of Damage or Corrosion

DI 5000 FH 5000 FH

72-50-00-11 Special Detailed Inspection of the C-Sump Drain for Oil Coking SDI 500 FH 500 FH 72-52-00-01 Special Detailed Inspection of the Engine Stage 1 and 2 Rotor Blades using

BorescopeSDI 3000 EH 3000 EH

72-52-00-03-1 Discard of the Engine High Pressure Turbine Rotor Stage 1 Disc DS Refer to Note Refer to Note LIFE Notes 1, 972-52-00-03-2 Discard of the Engine High Pressure Turbine Rotor Stage 2 Disc DS Refer to Note Refer to Note LIFE Notes 1, 972-52-00-03-3 Discard of the Engine High Pressure Turbine Rotor Balance Piston Seal DS Refer to Note Refer to Note LIFE Notes 1, 972-52-00-03-4 Discard of the Engine High Pressure Turbine Rotor HPT Shaft DS Refer to Note Refer to Note LIFE Notes 1, 972-52-00-03-5 Discard of the Engine High Pressure Turbine Rotor Outer Torque Coupling DS Refer to Note Refer to Note LIFE Notes 1, 972-52-00-03-6 Discard of the Engine High Pressure Turbine Rotor Inner Torque Coupling DS Refer to Note Refer to Note LIFE Notes 1, 972-53-00-01 Detailed Inspection of the Exterior of Engine Turbine Transition Duct DI 5000 FH 5000 FH 72-55-00-03-1 Discard of the Engine Low Pressure Turbine Rotor Turbine Rear Shaft DS Refer to Note Refer to Note LIFE Notes 1, 972-55-00-03-2 Discard of the Engine Low Pressure Turbine Rotor Stage 3 Disc DS Refer to Note Refer to Note LIFE Notes 1, 972-55-00-03-3 Discard of the Engine Low Pressure Turbine Rotor Stage 3/4 Disc DS Refer to Note Refer to Note LIFE Notes 1, 972-55-00-03-4 Discard of the Engine Low Pressure Turbine Rotor Stage 4 Disc DS Refer to Note Refer to Note LIFE Notes 1, 972-55-00-03-5 Discard of the Engine Low Pressure Turbine Rotor Stage 4/5 Disc DS Refer to Note Refer to Note LIFE Notes 1, 972-55-00-03-6 Discard of the Engine Low Pressure Turbine Rotor Stage 5 Disc DS Refer to Note Refer to Note LIFE Notes 1, 972-55-00-03-7 Discard of the Engine Low Pressure Turbine Rotor Stage 5/6 Seal DS Refer to Note Refer to Note LIFE Notes 1, 972-55-00-03-8 Discard of the Engine Low Pressure Turbine Rotor Stage 6 Disc DS Refer to Note Refer to Note LIFE Notes 1, 972-55-00-03-9 Discard of the Engine Low Pressure Turbine Rotor Drive Cone DS Refer to Note Refer to Note LIFE Notes 1, 972-56-00-01 General Visual Inspection of the Engine Exhaust Centerbody for Security or

Evidence of Cracks, Fragmentation, Thermal Deformation, or DamageGVI 500 FH 500 FH

72-60-00-01 General Visual Inspection of the Engine Common Collection Drain for Excessive Fluids

GVI 500 FH 500 FH

72-60-00-03 Detailed Inspection of the Engine Accessory Gearbox Mounts and Accessories for Condition and Security

DI 5000 FH 5000 FH

73-11-01-01 Detailed Inspection of the Engine Fuel Pump Housing for Evidence of Cracks or Mechanical Damage

DI 10000 FH 10000 FH

73-11-03-01 Discard the Engine Fuel Filter Element DS 2000 FH 2000 FH 73-11-03-03 Visual Check of the Engine Fuel Filter Mechanical Actual Bypass Indicator VC 1000 FH 1000 FH 73-11-09-01 General Visual Inspection of the Engine Fuel Manifold for Evidence of Leakage,

Cracks, or Mechanical Damage. Inspect Fuel Fittings for SecurityGVI

2000 FH 2000 FH

73-11-11-01 Special Detailed Inspection of the Engine Fuel Injectors for Evidence of Contamination (Coking) using Borescope

SDI 3000 EH 3000 EH




73-21-01-01 Detailed Inspection of the Engine Fuel Control for Evidence of Cracks, Mechanical Damage, Loose Fittings, or Fuel Leakage

DI 4000 FH 4000 FH EFFECTIVITY: Pre GE CF34-AL SB 73-0027 and Pre GE CF34-AL SB 73-0029, or Pre GE CF34-AL SB 73-0030

73-21-01-03 General Visual Inspection of the Engine BROWN ELECTRICAL CABLE (W9) for Condition and Security

GVI 5000 FH 5000 FH

73-21-01-09 Detailed Inspection of the Engine Fuel Control for Evidence of Cracks, Mechanical Damage, Loose Fittings, or Fuel Leakage

DI 5000 FH 5000 FH EFFECTIVITY: Post GE CF34-AL SB 73-0027 and Post GE CF34-AL SB 73-0029, or Post GE CF34-AL SB 73-0030

76-11-00-01 General Visual Inspection of the Throttle Quadrant, Engine and Throttle Control Cable for Condition and Security of Installation in Maximum Power and Shutoff Positions

GVI20000 FH 20000 FH

76-11-00-03 Functional Check of the Micro Switches of the Throttle Quadrant Adjustable Cam Switch Unit (ACSU)

FC 5000 FH 5000 FH

76-11-00-05 Functional Check of the Throttle Control System FC 10000 FH 10000 FH 76-11-00-09 Functional Check of the Throttle Lockout System FC 5000 FH 5000 FH 76-11-00-11 Functional Check of the Gearbox Assembly FC 8000 FH 8000 FH 76-11-00-13 Special Detailed Inspection Throttle gear box for gear tooth wear SDI 5000 FH 5000 FH Note: 4, EFFECTIVITY: P/N 2100140−01078-11-00-01 Detailed Inspection of the Engine Exhaust Nozzle Assembly for Cracks, Hot

Spots or DistortionDI 10000 FH 10000 FH

78-30-00-03 Functional Check of the Thrust Reverser System and PDU FC 4000 FH 4000 FH 78-30-00-05 Lubrication of the Thrust Reverser System LU 4000 FH 4000 FH 78-30-00-07 Detailed Inspection of the Thrust Reverser Components, Support Fittings, and

Attaching HardwareDI 2500 FH 2500 FH

78-30-00-09 Lubrication of the Thrust Reverser Tracks and Ball Screw Actuators LU 500 FH 500 FH 79-11-01-01 Detailed Inspection of the Engine Oil Tank Assembly for Cracks and Leakage

Interface FittingsDI 2000 FH 2000 FH

79-11-01-03 Service the Engine Oil Tank SV16 FH 16 FH

EFFECTIVITY: Task in not required if oil quantity indicating system installed. Mx Control will track this item for A/C that do not have the oil quantity indicating system installed.

79-12-00-01 Service the Oil Replenishment Tank SV 3 DY 3 DY 79-21-01-01 Detailed Inspection of the C-Sump Scavenge Screen Fittings In the Lube and

Scavenge Pump (Ports No. 3 and No. 4) for Coked Oil Build-UpDI 4000 FH 4000 FH EFFECTIVITY: Pre GE CF34-AL SB 79-0018

79-21-05-01 Visual Check of the Engine Oil Filter Impending Bypass Indicator for Filter Status

VC 1000 FH 1000 FH

79-21-05-03 Functional Check of the Engine Oil Filter Impending Bypass Sensor FC 5000 FH 5000 FH 79-21-05-05 Discard the Engine Oil Filter Element DS 2000 FH 2000 FH 79-21-09-01 Operational Check of the Engine Master Chip Detector OP 5000 FH 5000 FH 80-11-00-01 Discard and Renew Air Turbine Starter Oil DS 1000 FH 1000 FH 80-11-00-03 Detailed Inspection of the Air Turbine Starter Magnetic Drain Plug Chip Detector DI 1000 FH 1000 FH

80-11-00-05 Detailed Inspection of the Air Turbine Starter Oil Level at Filling Port DI 500 FH 500 FH


Chapter 3Structural Program


Structural Program

IntroductionThe section following contains the various inspection tasks that encompass the Structural Inspection tasks. The Structures Program is to be used in conjunction withthe Zonal Program. These tasks are defined as General Visual Inspections (GVI), Detailed Visual Inspections (DI/DVI), and Special Detailed Inspections (SDI). Theyare performed to ensure the inherent safety and reliability levels of the equipment. They also ensure that the safety and reliability of items are restored to their inherentlevels when deterioration has occurred.

Program NotesNOTE 1 The original MSG-3 analysis of this SSI identified a task to inspect for possible Accidental Damage. This task, however, was superceded by

the more conservative Environmental Damage task.

NOTE 2 The original MSG-3 analysis of this SSI identified a task to inspect for possible Environmental Damage. This task, however, was supercededby the more conservative Accidental Damage task.

NOTE 3 The RJ Damage Tolerance analysis has identified this task as an Airworthiness Limitation item. Therefore, the task cannot be changed(modified, deleted, or escalated) without the approval of Transport Canada Engineering. For the definitions of inspection intervals refer tothe indicated AWL in the Structural Airworthiness Limitations, Part 2, Appendix B of the MRM.

NOTE 4 The original MSG-3 analysis of this SSI yielded no task interval (double asterisk in either the Accidental or Environmental analysis). Thistask was transferred to the Zonal Program.

NOTE 5 Deleted

NOTE 6 No Aircraft Maintenance Manual reference is given for this task, because the task is precluded by the Zonal Program task referenced.





• Threshold - Indicates the maximum specified interval for the scheduled task of that item. Intervals are specified in calendar months unless indicatedotherwise

• Repeat - Identifies the repeat interval for the scheduled task. Intervals are specified in calendar months unless indicated otherwise


Chapter 3Structural Program



Maintenance Time Limitations Manual CRJ200 Chapter 3: Structures


52-11-02-01 Detailed Inspection of the Passenger Door Pin Fittings and attachments DI 48 MO 48 MO 52-21-02-01 Detailed Inspection of the Overwing Emergency Exit Latch Fittings and Door Stops DI 48 MO 48 MO Note 1

52-22-02-01 Detailed Inspection of the Crew Escape Hatch Pin Fitting and Stop Brackets DI 48 MO 48 MO 52-22-03-01 Detailed Inspection of the Crew Escape Hatch Stop Support Structure DI 96 MO 48 MO 52-31-02-01 Detailed Inspection of the Cargo Door Stop Fittings DI 48 MO 48 MO 52-41-02-01 Detailed Inspection of the Service Door Stops DI 72 MO 72 MO 52-42-02-01 Detailed Inspection of the Avionics Compartment Door Stops DI 72 MO 72 MO 52-42-03-01 Detailed Inspection of the Avionics Compartment Door Stop Support Structure DI 48 MO 48 MO 53-11-01-01 Detailed Inspection of the Station FS 169.0 and FS 193.0 Frames DI 72 MO 72 MO Note 253-11-05-01 Detailed Inspection of the Windshield Side Post Support DI 96 MO 72 MO 53-11-06-01 Detailed Inspection of the Flight Compartment Roof Internal Structure DI 72 MO 72 MO 53-11-07-01 Detailed Inspection of the Crew Escape Hatch Stop Fittings on Fuselage DI 96 MO 72 MO 53-11-09-01 Detailed Inspection of the FS 280.0 Bulkhead and Frame DI 72 MO 72 MO 53-11-11-01 Detailed Inspection of the Flight Compartment Floor Panels DI 72 MO 72 MO 53-11-11-02 Detailed Inspection of the Flight Compartment Floor - Seat Rails DI 48 MO 24 MO 53-11-15-01 Detailed Inspection of the forward Jacking Fitting at FS 278.00 DI 48 MO 48 MO 53-11-16-01 Detailed Inspection of the Windshield and Side Window Frames and Posts DI 72 MO 72 MO Note 253-11-17-01 Detailed Inspection of the Side Post Straps and Windshield/ Side Window Retainers DI 24 MO 24 MO Note 2

53-11-18-01 Detailed Inspection of the Nose Landing Gear (NLG) Trunnion Fitting and Diagonal Member

DI 48 MO 48 MO

53-11-19-01 Detailed Inspection of the Nose Landing Gear (NLG) Wheel Well Internal Box Structure FS 169 to FS 235

DI 48 MO 48 MO

53-21-02-02 Detailed Inspection of the Passenger Door Cutout Frames FS 310 and FS 349, and Interior Backup Structure (Exposed Areas)

DI 24 MO 24 MO

53-21-03-01 Detailed Inspection of the Passenger Door Fittings On Fuselage DI 96 MO 72 MO 53-21-04-01 Detailed Inspection of the Passenger Door Hinge On Fuselage DI 48 MO 48 MO 53-21-05-01 Detailed Inspection of the Fuselage Skin around Passenger Door Cutout DI 48 MO 48 MO Note 253-21-06-01 Detailed Inspection of the Fuselage Skin around Service Door Cutout DI 72 MO 48 MO Note 253-21-07-01 Detailed Inspection of the Service Door Fittings On Fuselage DI 72 MO 72 MO 53-21-08-02 Detailed Inspection of the Service Door Side Frames, Sills, and Back-Up Structure

(Exposed Surfaces)DI 48 MO 48 MO

53-21-09-01 Detailed Inspection of the Avionics Compartment Door Fittings On Fuselage DI 48 MO 48 MO Note 253-21-12-01 Detailed Inspection of the Side Seat Rail Structure forward of FS 409 DI 96 MO 48 MO 53-21-13-01 Detailed Inspection of the Internal Skin Panels, Frames and Stringers Above Floor

from FS 280 to FS 409DI 96 MO 72 MO

53-21-17-01 Detailed Inspection of the Exterior Lower Skin Panels, FS 280-FS 409 and Str17 to Bottom Centerline

DI 48 MO 48 MO Note 2

53-21-18-01 Detailed Inspection of the forward Water Servicing Cutout and Internal Box Structure DI 72 MO 72 MO

Revision 1 / April 15, 2008 Chapter 3: Structures 1 of 6



53-41-02-01 Detailed Inspection of the Side Seat Rail Structure FS 409.0 to FS 409.0 + 128.0 DI 96 MO 48 MO 53-41-03-01 Detailed Inspection of the Internal Skin Panels, Frames and Stringers Above Floor, FS

409.0 to FS 409.0 + 128.0DI 96 MO 72 MO

53-41-07-02 Detailed Inspection of the External Lower Skin Panel FS 4090 to FS 409.0 + 128.0, Str 20 to Bottom Centerline (Area Under Fairing)

DI 96 MO 72 MO

53-41-10-01 Detailed Inspection of the Interior Skin Panels, Frames and Stringers Above Floor, FS409 + 128 to FS559.0 Str 7 to top Centerline

DI 96 MO 72 MO

53-41-12-01 Detailed Inspection of the Internal Skin Panels, Frames, and Stringers, FS 409 + 128 to FS 559, Str 7 to Floor

DI 96 MO 72 MO

53-41-14-01 Detailed Inspection of the Fuselage Frame FS 409 + 128 Above Floor Level DI 96 MO 72 MO 53-41-17-01 Detailed Inspection of the Fuselage Frame FS 559 Above Floor DI 96 MO 72 MO 53-41-25-01 Detailed Inspection of the Frame FS 424 Above Floor DI 96 MO 72 MO 53-41-27-01 Detailed Inspection of the Frame FS 449.85 Above Floor DI 96 MO 72 MO 53-41-28-01 Detailed Inspection of the Frame FS 473.15 Above Floor DI 96 MO 72 MO 53-41-30-01 Detailed Inspection of the Frame FS513 Above Floor DI 96 MO 72 MO 53-41-31-01 Detailed Inspection of the Frame FS 513 Below Floor DI 96 MO 72 MO 53-41-41-01 Detailed Inspection of the Main Landing Gear (MLG) Uplock Structure FS 513 to FS

559DI 48 MO 48 MO Note 2

53-41-43-01 Detailed Inspection of the Side Seat Rail Structure, FS 409 + 128 to FS 559 DI 96 MO 48 MO 53-41-45-01 Detailed Inspection of the Side Seat Rail Structure Aft of FS 559 DI 96 MO 48 MO 53-41-46-01 Detailed Inspection of the Interior Skin Panels, Frames and Stringers Above Floor, FS

559 to FS 559 + 80DI 96 MO 72 MO

53-41-50-01 Detailed Inspection of the Exterior Lower Skin Panel, FS 559 to FS 559 + 112, Str 20 to Bottom Centerline

DI 96 MO 72 MO

53-41-52-01 Detailed Inspection of the Aft Lavatory Servicing Point Local Structure DI 48 MO 48 MO Note 253-41-53-01 Detailed Inspection of the Overwing Emergency Exit Stop Fittings On Fuselage DI 48 MO 48 MO 53-61-01-01 Detailed Inspection of the Rear Pressure Bulkhead Vertical Stiffeners DI 48 MO 48 MO 53-61-02-01 Detailed Inspection of the Rear Pressure Bulkhead Web Aft Side DI 96 MO 72 MO 53-61-12-01 Detailed Inspection of the Engine Pylon Splice Angle at FS 625.3 Between Str 9 and

10DI 96 MO 72 MO

53-61-21-01 Detailed Inspection of the Cargo Door Stop Fittings On Fuselage DI 18 MO 18 MO Note 253-61-23-01 Detailed Inspection of the Interior Skin Panels, Frames and Stringers Above Floor, FS

559 + 80 to FS 621DI 96 MO 72 MO

53-61-24-01 Detailed Inspection of the Engine Aft Mount Spars at Fuselage FS 672.20 and FS 682 DI 72 MO 72 MO

53-61-25-01-1 Detailed Inspection of the Engine Support Beam Structure DI 48 MO 48 MO Pre Modsum TC601R15054 or Pre SB 601R-53-059 Rev A or later

53-61-25-01-2 Detailed Inspection of the Engine Support Beam Structure DI 72 MO 72 MO Post Modsum TC601R15054 or Post SB 601R-53-059 Rev A or later

53-61-26-01 Detailed Inspection of the Engine forward Mount Spar at Frame FS 625.30 DI 96 MO 72 MO 53-61-27-01 Detailed Inspection of the Lower Transverse Beam Structure DI 96 MO 48 MO




53-61-29-01 Detailed Inspection of the Interior Lower Skin Panels, Frames and Stringers, FS 621 toFS 755, Str 20 to Bottom Centerline


53-61-30-01 Detailed Inspection of the Aft Equipmentment Compartment Door Cutout Interior Surrounding Structure


53-61-31-01 Detailed Inspection of the FS 755 Frame Structure forward Face DI 96 MO 72 MO 53-61-32-01 Detailed Inspection of the Exterior Skin Around Cargo Door Cutout DI 24 MO 24 MO Note 253-61-34-01 Detailed Inspection of the APU Inlet Door Cutout Interior Surrounding Structure DI 72 MO 72 MO Note 253-61-36-01 Detailed Inspection of the Exterior Skin Around APU Exhaust DI 48 MO 48 MO Note 253-61-39-01 Detailed Inspection of the Exterior Lower Skin Panel, FS 559 + 112 to FS 755 and Str

20 to Bottom CenterlineDI 24 MO 24 MO Note 2

53-71-01-01 Detailed Inspection of the Frame FS 755.0 Frame Structure Aft Side Above WL 125.0 DI 96 MO 72 MO

53-71-05-01 Detailed Inspection of the Vertical Stabilizer Front Spar attachment Fittings at Fuselage Frame FS 755.0

DI 48 MO 48 MO

53-71-07-01 Detailed Inspection of the FS 755 Frame Structure Aft Side Below WL 125 DI 96 MO 48 MO 53-71-08-01 Detailed Inspection of the Interior Structure from FS 755 to VS 67.5% DI 24 MO 24 MO Note 253-71-10-01 Detailed Inspection of the VS 67.5% Frame Structure Aft Side DI 96 MO 48 MO 53-71-12-01 Detailed Inspection of the Exterior Skin Panels of the Fuselage/Stabilizer Section, FS

755 to VS 67.5%DI 24 MO 24 MO Note 2

54-51-01-01 Detailed Inspection of the forward Engine Mount Spar Assembly DI 48 MO 48 MO Note 254-51-02-02 Detailed Inspection of the Pylon Box External Skins DI 96 MO 72 MO 54-51-03-01 Detailed Inspection of the Pylon Canted Ribs and Drag Braces DI 96 MO 72 MO 55-11-01-01 Detailed Inspection of the Bathtub Fitting On Center Section of Upper Skin DI 96 MO 72 MO 55-11-02-01 Detailed Inspection of the Screwjack attach Fittings DI 96 MO 72 MO 55-11-03-01 Detailed Inspection of the Front Spar Splice Assembly DI 96 MO 72 MO 55-11-04-01 Detailed Inspection of the Front Spar Assembly DI 96 MO 72 MO 55-11-05-01 Detailed Inspection of the Stringers (Outside PCU Bay) DI 96 MO 72 MO 55-11-05-02 Detailed Inspection of the Stringers (In PCU Bay) DI 72 MO 72 MO 55-11-06-01 Detailed Inspection of the Rear Spar Splice DI 96 MO 72 MO 55-11-07-01 Detailed Inspection of the Rear Spar Assembly DI 72 MO 72 MO 55-11-07-02 Detailed Inspection of the Rear Spar Assembly DI 96 MO 72 MO 55-11-08-01 Detailed Inspection of the Aft Centerline Rib (Y-Fitting) DI 96 MO 72 MO 55-11-09-01 Detailed Inspection of the forward Centerline Rib DI 96 MO 72 MO 55-11-10-01 Detailed Inspection of the Rib BL 6.0 DI 96 MO 72 MO 55-11-12-01 Detailed Inspection of the Upper Skin Splice, RBL 6.0 to LBL 6.0 (Exterior and Interior) DI 96 MO 72 MO

55-11-14-01 Detailed Inspection of the Lower Skin Splice, RBL 6.0 to LBL 6.0 (Exterior and Interior) DI 72 MO 72 MO

55-11-15-01 Detailed Inspection of the Elevator Hinge Fittings On Stabilizer DI 48 MO 48 MO Note 255-11-16-02 Detailed Inspection of the Elevator Center and Outboard Hinge Backup Fittings On

Horizontal StabilizerDI 96 MO 72 MO




55-11-17-01 Detailed Inspection of the PCU attachment Fittings DI 48 MO 48 MO Note 255-11-18-01 Detailed Inspection of the Flutter Damper attachment Fittings DI 72 MO 72 MO Note 155-11-19-01 Detailed Inspection of the Pivot Fitting DI 96 MO 72 MO 55-11-20-01 Detailed Inspection of the Horizontal Stabilizer Hinge Ribs DI 96 MO 72 MO 55-11-20-02 Detailed Inspection of the Horizontal Stabilizer Hinge Ribs (Inboard and Center Wings

Only)DI 48 MO 48 MO

55-11-21-01 Detailed Inspection of the Horizontal Stabilizer Interior Structure ( Outside Access Bays)

DI 96 MO 72 MO

55-11-21-02 Detailed Inspection of the Horizontal Stabilizer Interior Structure ( Inside Access Bays) DI 48 MO 48 MO

55-21-01-01 Detailed Inspection of the Elevator Front Spar Assembly DI 96 MO 72 MO 55-21-03-01 Detailed Inspection of the Elevator Hinge Ribs DI 96 MO 72 MO 55-21-04-01 Detailed Inspection of the Elevator Hinge Fittings DI 72 MO 72 MO Note 155-21-05-01 Detailed Inspection of the Elevator Hinge Backup Fittings DI 96 MO 72 MO 55-21-06-01 Detailed Inspection of the Elevator Rear Spar DI 96 MO 72 MO 55-21-07-01 Detailed Inspection of the Elevator Interior Structure DI 96 MO 72 MO 55-31-01-01 Detailed Inspection of the Front Spar to Fuselage attach Fitting DI 48 MO 48 MO 55-31-02-01 Detailed Inspection of the Front Spar to Fuselage Splice Strap DI 96 MO 72 MO 55-31-03-01 Detailed Inspection of the Front Spar forward Face DI 96 MO 72 MO 55-31-05-01 Detailed Inspection of the Rear Spar Aft Face DI 96 MO 72 MO 55-31-08-01 Detailed Inspection of the Vertical Stabilizer Access Panel Cutouts DI 48 MO 48 MO Note 255-31-09-01 Detailed Inspection of the Vertical Stabilizer Stringer Extension Splice VS 31.875% at

Rib 2 and VS 55.265% at Rib 3DI 96 MO 72 MO

55-31-10-01 Detailed Inspection of the top Canted Rib DI 96 MO 72 MO 55-31-11-01 Detailed Inspection of the Horizontal Stabilizer Pivot Fittings on Vertical Stabilizer DI 48 MO 48 MO 55-31-12-01 Detailed Inspection of the Horizontal Stabilizer Trim Actuator Pivot Structure DI 96 MO 72 MO 55-31-13-01 Detailed Inspection of the Vertical Stabilizer Interior DI 72 MO 72 MO Note 255-31-14-01 Detailed Inspection of the Rudder Hinge Fittings on Vertical Stabilizer DI 96 MO 72 MO 55-41-02-01 Detailed Inspection of the Rudder Leading Edge DI 96 MO 72 MO 55-41-03-01 Detailed Inspection of the Rudder Hinge Fitting Arms DI 96 MO 72 MO 55-41-04-01 Detailed Inspection of the Rudder Internal Structure DI 96 MO 72 MO 57-21-02-01 Detailed Inspection of the Aft Face of Center Wing Front Spar Between LBL 45.0 and

RBL 45.0DI 96 MO 72 MO

57-21-03-01 Detailed Inspection of the forward Face of Center Wing Rear Spar Between LBL 45.0 and 45.0

DI 96 MO 72 MO

57-21-06-01 Detailed Inspection of the Exterior Surface of Center Wing Lower Plank Between LBL 45.0 and RBL 45.0

DI 96 MO 72 MO

57-21-07-01 Detailed Inspection of the Interior Upper Wing Plank In Center Wing, LBL 45.0 to RBL 45.0 and RBL 45.0

DI 96 MO 72 MO

57-21-08-01 Detailed Inspection of the Interior Lower Wing Plank In Center Wing, LBL 45.0 to RBL 45.0

DI 96 MO 72 MO




57-21-09-01 Detailed Inspection of the Ribs In the Center Wing, LBL 45.0 to RBL 45.0 DI 96 MO 72 MO 57-21-11-01 Detailed Inspection of the Aft Face of Wing Front Spar Between BL 45.0 and Canted

WS314.5DI 96 MO 72 MO

57-21-12-01 Detailed Inspection of the forward Face of Wing Rear Spar Between BL 45.0 and WS 314.5

DI 96 MO 72 MO

57-21-13-01 Detailed Inspection of the Aft Face of Wing Rear Spar Between WS 48.0 and WS 389.0


57-21-14-01 Detailed Inspection of the Interior Upper Wing Plank Between Wing Spars from BL 45.0 to Canted WS314.5

DI 96 MO 72 MO

57-21-15-01 Detailed Inspection of the Interior Lower Wing Plank Between Wing Spars from BL 45.0 to WS314.5

DI 96 MO 72 MO

57-21-16-01 Detailed Inspection of the Wing Ribs Between BL 45.0 and Canted WS 314.5 DI 96 MO 72 MO 57-21-17-01 Detailed Inspection of the Interior Structure In the Dry Bay Between Canted WS 314.5

and WS353.0DI 48 MO 48 MO Note 2

57-21-18-01 Detailed Inspection of the Interior Structure In the Wing Plug, WS 353.0 to WS 389.0 DI 96 MO 72 MO

57-21-19-01 Detailed Inspection of the Exterior Surface of the Upper Wing Plank Between BL 47.0 and Canted WS314.5


57-21-20-01 Detailed Inspection of the Exterior Surface of the Lower Wing Plank Between BL 45.0 and Canted WS 314.5

DI 96 MO 72 MO

57-21-21-01 Detailed Inspection of the Exterior Surface of the Upper Wing Skin Between Canted WS314.5 and WS389.0


57-21-22-01 Detailed Inspection of the Exterior Surface of the Lower Wing Skin Between Canted WS314.5 and WS389.0


57-21-23-01 Detailed Inspection of the Auxiliary Spar Assembly DI 48 MO 48 MO Note 257-21-24-01 Detailed Inspection of the Interior Wing Planks and Batt Ribs Between Rear Spar and

Auxiliary Spar WS48.0 to WS127.5DI 96 MO 72 MO

57-21-25-01-1 Detailed Inspection of the LH Main Landing Gear (MLG) Trunnion Strap and Adjacent Wing Skin

DI 72 MO 72 MO

57-21-25-01-2 Detailed Inspection of the RH Main Landing Gear (MLG) Trunnion Strap and Adjacent Wing Skin

DI 72 MO 72 MO

57-21-26-01 Detailed Inspection of the Main Landing Gear (MLG) Trunnion Fitting DI 96 MO 72 MO 57-21-27-01 Detailed Inspection of the Main Landing Gear (MLG) Mounting Fittings On Rib WS

65.75DI 96 MO 72 MO

57-21-34-01 Detailed Inspection of the Flap Box attach Fittings - Inboard Flaps DI 48 MO 48 MO Note 257-21-35-01 Detailed Inspection of the Flap Box attach Fittings - Outboard Flaps DI 48 MO 48 MO Note 257-21-36-01 Detailed Inspection of the Aileron Damper attach Fitting DI 72 MO 72 MO Note 157-21-37-01 Detailed Inspection of the Wing Jacking Fitting DI 96 MO 72 MO 57-31-02-01 Detailed Inspection of the Wing Tip Spars and Ribs DI 72 MO 72 MO 57-51-01-01 Detailed Inspection of the Inboard Ground Spoiler Hinge Fittings DI 48 MO 48 MO Note 257-51-02-01 Detailed Inspection of the Outboard Ground Spoiler Hinge Fittings DI 48 MO 48 MO Note 2




57-51-03-01 Detailed Inspection of the Flight Spoiler Hinge Fittings DI 48 MO 48 MO Note 257-51-04-01 Detailed Inspection of the Spoileron Hinge Fittings DI 48 MO 48 MO Note 257-51-05-01 Detailed Inspection of the Aileron Hinge Fittings DI 48 MO 48 MO Note 257-52-02-01 Detailed Inspection of the Inboard Flap Lower Skin - Exterior DI 48 MO 48 MO Note 257-52-03-01 Detailed Inspection of the Inboard Flap Front Spar DI 96 MO 72 MO 57-52-04-01 Detailed Inspection of the Inboard Flap Vane Actuator Support Structure DI 96 MO 48 MO 57-52-06-01 Detailed Inspection of the Inboard Flap Hinge Support Ribs DI 96 MO 48 MO 57-52-07-01 Detailed Inspection of the Inboard Flap Hinge Lug Plates DI 96 MO 48 MO 57-52-08-01 Detailed Inspection of the Inboard Flap Hinge Arms DI 72 MO 72 MO 57-52-14-01 Detailed Inspection of the Inboard Flap Vane Actuator Sliding Beam DI 48 MO 24 MO 57-52-15-01 Detailed Inspection of the Inboard Flap Vane Actuator Carriages DI 96 MO 48 MO 57-52-17-01 Detailed Inspection of the Inboard Flap Vane Skins DI 48 MO 48 MO Note 257-52-19-01 Detailed Inspection of the Inboard Flap Vane Mounting Structure DI 96 MO 72 MO 57-52-20-01 Detailed Inspection of the Inboard Flap Internal Structure DI 96 MO 72 MO 57-53-04-01 Detailed Inspection of the Outboard Flap Vane Mounts (Exposed Areas Only) DI 96 MO 72 MO 57-53-05-01 Detailed Inspection of the Outboard Flap Inboard Hinge Interior Support Structure DI 96 MO 72 MO 57-53-07-01 Detailed Inspection of the Outboard Flap Inboard Hinge Lug Fittings DI 96 MO 72 MO 57-53-10-01 Detailed Inspection of the Outboard Flap Inboard Hinge Arm Assembly DI 72 MO 48 MO 57-53-12-01 Detailed Inspection of the Outboard Flap Center Hinge Lug Fittings DI 72 MO 72 MO 57-53-13-01 Detailed Inspection of the Outboard Flap Center Hinge Arm DI 72 MO 72 MO 57-53-15-01 Detailed Inspection of the Outboard Flap Outboard Hinge Interior Support Structure DI 96 MO 72 MO57-53-17-01 Detailed Inspection of the Outboard Flap Outboard Hinge Lug Fitting DI 96 MO 72 MO 57-53-20-01 Detailed Inspection of the Outboard Flap Outboard Hinge Arm Assembly DI 72 MO 48 MO 57-53-24-01 Detailed Inspection of the Outboard Flap Vane Mounting Structure DI 96 MO 72 MO 57-53-25-01 Detailed Inspection of the Outboard Flap Internal Structure DI 96 MO 72 MO 57-54-01-01 Detailed Inspection of the Inboard Flap Hinge Boxes DI 72 MO 48 MO 57-54-02-01 Detailed Inspection of the Outboard Flap Hinge Boxes DI 72 MO 48 MO 57-61-01-01 Detailed Inspection of the Aileron Center Fitting DI 96 MO 72 MO 57-61-04-01 Detailed Inspection of the Aileron Front Spar DI 72 MO 72 MO 57-61-05-01 Detailed Inspection of the Aileron Internal Structure DI 96 MO 72 MO 57-61-06-01 Detailed Inspection of the Aileron Hinge Fittings DI 48 MO 48 MO Note 257-71-01-01 Detailed Inspection of the Inboard Ground Spoiler Hinge Ribs DI 48 MO 48 MO Note 257-71-02-01 Detailed Inspection of the Inboard Ground Spoiler Skins and Spars DI 48 MO 48 MO Note 257-72-01-01 Detailed Inspection of the Outboard Ground Spoiler Hinge Ribs DI 48 MO 48 MO Note 257-72-02-01 Detailed Inspection of the Outboard Ground Spoiler Skins and Spars DI 48 MO 48 MO Note 257-73-01-01 Detailed Inspection of the Flight Spoiler Hinge Fittings DI 48 MO 48 MO Note 257-73-02-01 Detailed Inspection of the Flight Spoiler Skins and Spars DI 48 MO 48 MO Note 257-74-01-01 Detailed Inspection of the Spoileron Assembly DI 48 MO 48 MO Note 2


Chapter 4Zonal Maintenance Program


Zonal Maintenance Program

IntroductionThe following section contains the various inspection tasks that encompass the Zonal Inspection tasks. These tasks are defined as General Visual Inspections (GVI).They are performed to ensure the inherent safety and reliability levels of the equipment. They also ensure that the safety and reliability of items are restored to theirinherent levels when deterioration has been detected. Zonal Inspection tasks must be of sufficient depth to establish that any significant deterioration is identified andrectified to ensure that the general quality/condition of the area/zone is satisfactory until the next higher inspection becomes due.

Program NotesNOTE 1 No task selected. A zonal analysis was carried out, as a result of the ineffectiveness to conduct a General Visual Inspection (GVI), it was

determined that no suitable task can be performed for this zone.









Maintenance Time Limitations Manual CRJ200 Chapter 4: Zonal


32-700-01 General Visual Inspection of the External Nose Landing Gear Assembly GVI 5000 FH 5000 FH

32-700-02 General Visual Inspection of the External LH Main Landing Gear Assembly GVI 5000 FH 5000 FH

32-700-03 General Visual Inspection of the External RH Main Landing Gear Assembly

GVI 5000 FH 5000 FH

52-700-01 General Visual Inspection of the External LH Nose Landing Gear Door GVI 15000 FH 15000 FH 52-700-02 General Visual Inspection of the External RH Nose Landing Gear Door GVI 15000 FH 15000 FH 52-700-03 General Visual Inspection of the External Nose Landing Gear Aft Doors GVI 15000 FH 15000 FH

52-700-04 General Visual Inspection of the External LH Main Landing Gear Door GVI 5000 FH 5000 FH 52-700-05 General Visual Inspection of the External RH Main Landing Gear Door GVI 5000 FH 5000 FH 52-800-01 General Visual Inspection of the External Avionics Compartment Door GVI 5000 FH 5000 FH 52-800-02 General Visual Inspection of the Internal Main Avionics Compartment Door GVI 10000 FH 10000 FH

52-800-03 General Visual Inspection of the External Crew Escape Hatch GVI 10000 FH 10000 FH 52-800-04 General Visual Inspection of the Internal Crew Escape Hatch GVI 10000 FH 10000 FH 52-800-05 General Visual Inspection of the External Passenger Door GVI 5000 FH 5000 FH 52-800-06 General Visual Inspection of the Internal Passenger Door GVI 5000 FH 5000 FH 52-800-07 General Visual Inspection of the External LH and RH Overwing Emergency

ExitsGVI 10000 FH 10000 FH

52-800-08 General Visual Inspection of the Internal LH and RH Overwing Emergency Exits

GVI 10000 FH 10000 FH

52-800-09 General Visual Inspection of the External Cargo (Baggage) Compartment Door

GVI 5000 FH 5000 FH

52-800-10 General Visual Inspection of the Internal Cargo (Baggage) Compartment Door

GVI 5000 FH 5000 FH

52-800-11 General Visual Inspection of the External Service Door GVI 5000 FH 5000 FH 52-800-12 General Visual Inspection of the Internal Service Door GVI 10000 FH 10000 FH 53-100-01 General Visual Inspection of the External Radome GVI 10000 FH 10000 FH 53-100-02 General Visual Inspection of the Internal Radome GVI 15000 FH 15000 FH 53-100-03 General Visual Inspection of the External Fuselage Nose Skin FS 169.00

to FS 202.75, Below WL 79.50GVI 10000 FH 10000 FH

53-100-04 General Visual Inspection of the Internal LH Lower Nose Compartment GVI 5000 FH 5000 FH 53-100-05 General Visual Inspection of the Internal RH Lower Nose Compartment GVI 5000 FH 5000 FH 53-100-06 General Visual Inspection of the Internal Nose Wheel Well GVI 5000 FH 5000 FH 53-100-07 General Visual Inspection of the External Forward Fuselage, FS 202.75 to

FS 280.00, Below WL 79.50GVI 10000 FH 10000 FH

53-100-08 General Visual Inspection of the Internal LH Forward Avionics and Flight Controls Compartment

GVI 5000 FH 5000 FH

Revision 1 / April 15, 2008 Chapter 4: Zonal 1 of 5



53-100-09 General Visual Inspection of the Internal RH Forward Avionics and Flight Controls Compartment

GVI 10000 FH 10000 FH

53-100-10 General Visual Inspection of the External FWD/MID Fuselage, FS 280.00 to FS 409.00 + 80, Below WL 73.50

GVI 10000 FH 10000 FH

53-100-11 General Visual Inspection of the Internal LH Main Avionics Compartment GVI 10000 FH 10000 FH

53-100-12 General Visual Inspection of the Internal RH Main Avionics Compartment GVI 10000 FH 10000 FH

53-100-13 General Visual Inspection of the External MID Fuselage and Forward Wing to Fuselage Fairings, FS 409.00 + 80 to FS 409.00 + 128, Below WL 73.50

GVI10000 FH 10000 FH

53-100-14 General Visual Inspection of the Internal LH Forward ECS Compartment GVI 10000 FH 10000 FH

53-100-15 General Visual Inspection of the Internal RH Forward ECS Compartment GVI 10000 FH 10000 FH

53-100-16 General Visual Inspection of the External Overwing to Fuselage Panels, FS 409.00 + 128 + FS 559.00, Below WL 73.50

GVI 10000 FH 10000 FH

53-100-17 General Visual Inspection of the Internal LH Mid-Lower Fuselage Lower Pressure Floor, Excluding Center Wing

GVI 10000 FH 10000 FH

53-100-18 General Visual Inspection of the Internal RH Mid-Lower Fuselage Lower Pressure Floor, Excluding Center Wing

GVI 10000 FH 10000 FH

53-100-19 General Visual Inspection of the Internal LH Main Landing Gear Wheel Well

GVI 5000 FH 5000 FH

53-100-20 General Visual Inspection of the Internal RH Main Landing Gear Wheel Well

GVI 5000 FH 5000 FH

53-100-21 General Visual Inspection of the Internal Mid-Lower Fuselage Between Pressure Floor and Cabin Floor

GVI 10000 FH 10000 FH

53-100-22 General Visual Inspection of the External Aft Fuselage and Aft Wing to Fuselage Fairings, FS 559.00 to FS 621.00, Below WL 73.50

GVI 10000 FH 10000 FH

53-100-23 General Visual Inspection of the Internal LH Aft ECS Compartment GVI 10000 FH 10000 FH 53-100-26 General Visual Inspection of the Internal RH Aft ECS Compartment GVI 10000 FH 10000 FH 53-200-01 General Visual Inspection of the External Fuselage Nose Skin FS 169.00

to FS 202.75, Above WL 79.50GVI 10000 FH 10000 FH

53-200-02 General Visual Inspection of the Internal LH Forward Equipment Compartment

GVI 12000 FH 12000 FH

53-200-03 General Visual Inspection of the Internal RH Forward Equipment Compartment

GVI 12000 FH 12000 FH

53-200-04 General Visual Inspection of the External Forward Fuselage, FS 202.75 to FS 280.00, Above WL 79.50

GVI 5000 FH 5000 FH

53-200-05 General Visual Inspection of the Internal LH Flight Compartment GVI 5000 FH 5000 FH 53-200-06 General Visual Inspection of the Internal RH Flight Compartment GVI 5000 FH 5000 FH




53-200-07 General Visual Inspection of the External FWD/MID Fuselage, FS 280.00 to FS 349.00, Above WL 73.50

GVI 10000 FH 10000 FH

53-200-08 General Visual Inspection of the Internal LH Passenger Compartment, Entry Area

GVI 10000 FH 10000 FH

53-200-09 General Visual Inspection of the Internal RH Passenger Compartment, Galley Area

GVI 10000 FH 10000 FH

53-200-10 General Visual Inspection of the External Center Fuselage, FS 349.00 to FS 559.00 + 80, Above WL 73.50

GVI 10000 FH 10000 FH

53-200-11 General Visual Inspection of the Internal LH Passenger Compartment GVI 15000 FH 15000 FH 53-200-12 General Visual Inspection of the Internal RH Passenger Compartment GVI 15000 FH 15000 FH 53-200-30 General Visual Inspection of the External Aft Fuselage, FS 559.00 + 80 to

FS 621.00, Above WL 73.50GVI 10000 FH 10000 FH

53-200-31 General Visual Inspection of the Internal LH Cargo Compartment GVI 5000 FH 5000 FH 53-200-32 General Visual Inspection of the Internal RH Cargo Compartment GVI 5000 FH 5000 FH 53-300-01 General Visual Inspection of the External Aft Fuselage, FS 621.00 to FS

755.00GVI 5000 FH 5000 FH

53-300-02 General Visual Inspection of the Internal Aft Equipment Compartment GVI 5000 FH 5000 FH 53-300-03 General Visual Inspection of the External Aft Fuselage/Stabilizer Section GVI 10000 FH 10000 FH

53-300-04 General Visual Inspection of the Internal Aft Fuselage/Stabilizer Section GVI 10000 FH 10000 FH

53-300-05 General Visual Inspection of the External Tail Cone GVI 16000 FH 16000 FH 53-300-06 General Visual Inspection of the Internal Tail Cone GVI 20000 FH 20000 FH 54-400-01 General Visual Inspection of the External LH Pylon GVI 5000 FH 5000 FH 54-400-02 General Visual Inspection of the Internal LH Pylon - Leading Edge GVI 10000 FH 10000 FH 54-400-03 General Visual Inspection of the Internal LH Pylon - Mid Section GVI 5000 FH 5000 FH 54-400-04 General Visual Inspection of the Internal LH Pylon - Trailing Edge GVI 25000 FH 25000 FH 54-400-05 General Visual Inspection of the External RH Pylon GVI 5000 FH 5000 FH 54-400-06 General Visual Inspection of the Internal RH Pylon - Leading Edge GVI 10000 FH 10000 FH 54-400-07 General Visual Inspection of the Internal RH Pylon - Mid Section GVI 5000 FH 5000 FH 54-400-08 General Visual Inspection of the Internal RH Pylon - Trailing Edge GVI 25000 FH 25000 FH 55-300-01 General Visual Inspection of the External Vertical Stabilizer Assembly GVI 10000 FH 10000 FH 55-300-02 General Visual Inspection of the Internal Air Conditioning Ram Air GVI 20000 FH 20000 FH 55-300-03 General Visual Inspection of the Internal Vertical Stabilizer Leading Edge GVI 20000 FH 20000 FH

55-300-04 General Visual Inspection of the Internal Vertical Stabilizer GVI 10000 FH 10000 FH 55-300-05 General Visual Inspection of the Internal Vertical Stabilizer Tip GVI 10000 FH 10000 FH 55-300-07 General Visual Inspection of the External LH and RH Horizontal Stabilizer GVI 10000 FH 10000 FH

55-300-08 General Visual Inspection of the Internal LH and RH Horizontal Stabilizer Leading Edges

GVI 20000 FH 20000 FH




55-300-09 General Visual Inspection of the Internal LH and RH Horizontal Stabilizer GVI 10000 FH 10000 FH

55-300-10 General Visual Inspection of the Internal LH and RH Horizontal Stabilizer Tips

GVI 25000 FH 25000 FH

57-500-01 General Visual Inspection of the External LH Side of the Center Wing GVI 10000 FH 10000 FH 57-500-02 General Visual Inspection of the Internal LH Side of the Center Wing GVI 10000 FH 10000 FH 57-500-03 General Visual Inspection of the External LH Inboard Leading Edge GVI 10000 FH 10000 FH 57-500-04 General Visual Inspection of the Internal LH Inboard Leading Edge GVI 16000 FH 16000 FH 57-500-05 General Visual Inspection of the External LH Outboard Leading Edge GVI 10000 FH 10000 FH 57-500-06 General Visual Inspection of the Internal LH Outboard Leading Edge GVI 16000 FH 16000 FH 57-500-07 General Visual Inspection of the External LH Inboard Wings GVI 10000 FH 10000 FH 57-500-08 General Visual Inspection of the Internal LH Inboard Wing Fuel Tank GVI 10000 FH 10000 FH 57-500-09 General Visual Inspection of the External LH Outboard Wing GVI 10000 FH 10000 FH 57-500-10 General Visual Inspection of the Internal LH Outboard Wing Fuel Tank GVI 10000 FH 10000 FH 57-500-11 General Visual Inspection of the Internal LH Outboard Wing Dry Bay GVI 10000 FH 10000 FH 57-500-12 General Visual Inspection of the Internal LH Wing Between Rear Spar and

Auxiliary SparGVI 16000 FH 16000 FH

57-500-13 General Visual Inspection of the External LH Wingtip GVI 10000 FH 10000 FH 57-500-14 General Visual Inspection of the Internal LH Wingtip Extension GVI 20000 FH 20000 FH 57-500-16 General Visual Inspection of the External LH Inboard Wing Trailing Edge GVI 10000 FH 10000 FH

57-500-17 General Visual Inspection of the Internal LH Inboard Fixed Fairing GVI 10000 FH 10000 FH 57-500-21 General Visual Inspection of the External LH Outboard Wing Trailing Edge GVI 10000 FH 10000 FH

57-500-22 General Visual Inspection of the Internal LH Outboard Wing Trailing Edge GVI 10000 FH 10000 FH

57-500-27 General Visual Inspection of the Internal LH Aileron Shrouds GVI 10000 FH 10000 FH 57-600-01 General Visual Inspection of the External RH Side of the Center Wing GVI 10000 FH 10000 FH 57-600-02 General Visual Inspection of the Internal RH Side of the Center Wing GVI 10000 FH 10000 FH 57-600-03 General Visual Inspection of the External RH Inboard Leading Edge GVI 10000 FH 10000 FH 57-600-04 General Visual Inspection of the Internal RH Inboard Leading Edge GVI 16000 FH 16000 FH 57-600-05 General Visual Inspection of the External RH Outboard Leading Edge GVI 10000 FH 10000 FH 57-600-06 General Visual Inspection of the Internal RH Outboard Leading Edge GVI 16000 FH 16000 FH 57-600-07 General Visual Inspection of the External RH Inboard Wing GVI 10000 FH 10000 FH 57-600-08 General Visual Inspection of the Internal RH Inboard Wing Fuel Tank GVI 10000 FH 10000 FH 57-600-09 General Visual Inspection of the External RH Outboard Wing GVI 10000 FH 10000 FH 57-600-10 General Visual Inspection of the Internal RH Outboard Wing Fuel Tank GVI 10000 FH 10000 FH 57-600-11 General Visual Inspection of the Internal RH Outboard Wing Dry Bay GVI 10000 FH 10000 FH 57-600-12 General Visual Inspection of the Internal RH Wing Between Rear Spar and

Auxiliary SparGVI 16000 FH 16000 FH

57-600-13 General Visual Inspection of the External RH Wingtip GVI 10000 FH 10000 FH




57-600-14 General Visual Inspection of the Internal RH Wingtip Extension GVI 20000 FH 20000 FH 57-600-16 General Visual Inspection of the External RH Inboard Wing Trailing Edge GVI 10000 FH 10000 FH

57-600-17 General Visual Inspection of the Internal RH Inboard Fixed Fairing GVI 10000 FH 10000 FH 57-600-21 General Visual Inspection of the External RH Outboard Wing Trailing Edge GVI 10000 FH 10000 FH

57-600-22 General Visual Inspection of the Internal RH Outboard Wing Trailing Edge GVI 10000 FH 10000 FH

57-600-27 General Visual Inspection of the Internal RH Aileron Shrouds GVI 10000 FH 10000 FH 71-400-01 General Visual Inspection of the External LH Engine Nacelle GVI 5000 FH 5000 FH 71-400-02 General Visual Inspection of the Internal LH Engine Nose Cowl GVI 10000 FH 10000 FH 71-400-03 General Visual Inspection of the Internal LH Engine Nose Access Cowl GVI 15000 FH 15000 FH

71-400-04 General Visual Inspection of the Internal LH Engine Thrust Reverser torque Box

GVI 15000 FH 15000 FH

71-400-05 General Visual Inspection of the Internal LH Engine Translating Cowl GVI 15000 FH 15000 FH 71-400-06 General Visual Inspection of the Internal LH Engine Core Cowl GVI 5000 FH 5000 FH 71-400-07 General Visual Inspection of the Internal LH Engine Tailpipe GVI 5000 FH 5000 FH 71-400-08 General Visual Inspection of the External RH Engine Nacelle GVI 5000 FH 5000 FH 71-400-09 General Visual Inspection of the Internal RH Engine Nose Cowl GVI 10000 FH 10000 FH 71-400-10 General Visual Inspection of the Internal RH Engine Nose Access Cowl GVI 15000 FH 15000 FH

71-400-11 General Visual Inspection of the Internal RH Engine Thrust Reverser torque Box

GVI 15000 FH 15000 FH

71-400-12 General Visual Inspection of the Internal RH Engine Translating Cowl GVI 15000 FH 15000 FH 71-400-13 General Visual Inspection of the Internal RH Engine Core Cowl GVI 5000 FH 5000 FH 71-400-14 General Visual Inspection of the Internal RH Engine Tailpipe GVI 5000 FH 5000 FH


Chapter 5AWL Program


AWL Program

IntroductionThe section following contains the various maintenance and inspection tasks that encompass the AWL Inspection tasks. The AWL is further broke down into the followingtasks: Certification Maintenance Requirements (CMR), Structural Airworthiness Limitations, Life Limits (Structural and System Component), SupplementaryRequirements (SR), and Structural Repair Limitations (SRL). These tasks are defined as Detailed Visual Inspections (DI/DVI), Special Detailed Inspections (SDI), andDiscard Intervals (DIS). They are performed to ensure the inherent safety and reliability levels of the equipment. They also ensure that the safety and reliability of itemsare restored to their inherent levels when deterioration has occurred.

Program NotesNOTE 1 Interim value; Evaluation and test to continue.

NOTE 2 AC Motor Pump 601R75154-5 is replaced by 601R75154-7, which has no life limit.

NOTE 3 This task is against optional equipment and may not be installed on all aircraft.

NOTE 4 Detailed Visual or Special Detailed Inspection may be chosen. However, whichever inspection method is chosen, the method MUST beadhered to. An operator cannot alternate between either method.

NOTE 5 Return to vendor for required inspection.

NOTE 6 Aircraft that have the option of limiting the maximum take off weight (MTOW) to 52000 lb will apply the inspection program and life limit ofthe 53000 lb MTOW aircraft.

Additional NotesNOTE

One star CMRs (*) -The task and intervals specified are mandatory and cannot be changed, escalated, or deleted without the concurrenceof the applicable airworthiness authority.

Two star CMRs (**) -Task intervals may be adjusted in accordance with an operator’s approved escalation practices or an approved reliabilityprogram, but the tasks may not be changed or deleted without approval from he applicable airworthiness authority.




Chapter 5AWL Program



• Threshold - Indicates the maximum specified interval for the scheduled task of that item. Intervals are specified in flight cycles unless indicated otherwise

• Repeat - Identifies the repeat interval for the scheduled task. Intervals are specified in flight cycles unless indicated otherwise



Maintenance Time Limitations Manual CRJ200 Chapter 5: AWL


27-11-01a Discard of the Aileron Flutter Damper Shear Pin (Solid) DS 1534 FC 1534 FC LIFE Canadair P/N 600-10179-127-11-01b Discard of the Aileron Flutter Damper Shear Pin

(Counterbored)DS 5400 FC 5400 FC LIFE Canadair P/N 601R-10179-1

27-11-05 Task Deleted Sep 14/0727-11-06 Task Deleted Sep 14/0727-21-06 Task Deleted Sep 14/0727-31-01a Discard of the Elevator Flutter Damper Shear Pin (Grooved) DS 810 FC 810 FC LIFE P/N 601R24063-2501

27-31-01b Discard of the Elevator Flutter Damper Shear Pin (Counterbored)

DS 20000 FC 20000 FC LIFE P/N 601R24063-31

27-31-01c Discard of the Elevator Flutter Damper Shear Pin (Counterbored)

DS 20000 FC 20000 FC LIFE P/N 601R24063-31/S

27-31-01d Discard of the Elevator Flutter Damper Shear Pin (Counterbored)

DS 20000 FC 20000 FC LIFE P/N 601R24063-951

27-31-01e Discard of the Elevator Flutter Damper Shear Pin (Counterbored)

DS 20000 FC 20000 FC LIFE P/N 601R24063-953

27-31-01f Discard of the Elevator Flutter Damper Shear Pin (Counterbored)

DS 20000 FC 20000 FC LIFE P/N RNC C079033-1/375

27-31-02 Task Deleted Sep 14/0727-40-101 Special Detailed Inspection of the Horizontal Stabilizer Pitch

Trim Actuator - Screw Shaft and Gimble AssembliesSDI

40000 FC 40000 FC Note 5

27-40-102 Special Detailed Inspection of the Horizontal Stabilizer Pitch Trim Actuator - Pins

SDI 40000 FC 40000 FC Note 5

27-42-01 Discard of the Horizontal Stabilizer Trim Actuating System Actuator - Horizontal Stabilizer Trim (HSTA)

DS

19200 FH 19200 FH

LIFE Canadair P/N 601R92305-1 and 601R92305-3 Vendor P/N 8396-2 and 8396-3 NOTE: For HSTA with 18200 flight hours or more at the data of receipt of this Temporary Revision, remove and replace the HSTA within the next 1000 flight hours. NOTE: Airworthiness Directive issued.

27-51-10 Discard of the Flap Control System Sensor Unit - Flap Brake and Position (BPSU)

DS50000 FC 50000 FC

LIFE Canadair P/N 601R93105-11 Vendor P/N 855D100-11. Life Limit to be tracked in Part Master File in RPA.

27-53-01a Discard of the Flap Actuating Mechanism System Actuator - Inboard Flap

DS 12000 FH 12000 FH LIFE Note 1 Canadair P/N 601R93101-3 Vendor P/N 852D100-5

27-53-01b Discard of the Flap Actuating Mechanism System Actuator - Inboard Flap

DS 30000 FC 30000 FC LIFE TR 2B-2121 Note 1 Canadair P/N 601R93101-19 Vendor P/N 852D100-19

27-53-01c Discard of the Flap Actuating Mechanism System Actuator - Inboard Flap

DS 14666 FC 14666 FC LIFE TR 2B-2124 Note 1 Canadair P/N 601R93101-21 Vendor P/N 852D100-21

27-53-05a Discard of the Flap Actuating Mechanism System Actuator - Outboard Flap


27-53-05b Discard of the Flap Actuating Mechanism System Actuator - Outboard Flap


Revision 1 / April 15, 2008 Chapter 5: AWL 1 of 36



27-53-05c Discard of the Flap Actuating Mechanism System Actuator - Outboard Flap

DS 33333 FC 33333 FC LIFE Note 1 Canadair P/N 601R93103-19 Vendor P/N 853D100-19

27-53-05d Discard of the Flap Actuating Mechanism System Actuator - Outboard Flap


27-53-05e Discard of the Flap Actuating Mechanism System Actuator - Outboard Flap


27-53-05f Discard of the Flap Actuating Mechanism System Actuator - Outboard Flap


27-53-05g Discard of the Flap Actuating Mechanism System Actuator - Outboard Flap


27-53-05h Discard of the Flap Actuating Mechanism System Actuator - Outboard Flap


27-53-10 Discard of the Flap Actuating Mechanism System Shaft Assembly - Flexible Drive

DS 18000 FH 18000 FH LIFE Note 1 Canadair P/N 601R93106-101 Vendor P/N 857SD100-1

27-54-15a Task Deleted per Rev. 7 Part 2 MRM. P/N 601R14202-3 (Repaired unit only)27-54-15b Discard of the Inboard Flap Vane Actuator Assembly DS 40000 FC 40000 FC LIFE P/N 601R14202-327-54-15c Discard of the Inboard Flap Vane Actuator Assembly DS 40000 FC 40000 FC LIFE P/N 601R14202-528-24-01 Discard of the Auxiliary Power Unit (APU) Fuel Feed System

Cartridge - APU Fuel PumpDS 1800 AH 1800 AH LIFE Canadair P/N 601R62204-5 and 601R62204-7

Vendor P/N 228077-1 and 228077-229-11-03 Discard of the Hydraulic Systems No.1 and No.2 Pump - AC

Motor Driven (ACMP)DS 1200 FH 1200 FH LIFE Note 2 Canadair P/N 601R75154-5 Vendor P/N

84843132-11-102 Discard of the Trailing Arm DS

27500 FC 27500 FC

LIFE Canadair P/N 601R85001-7 and Vendor P/N 17084-103 Note: These lives are applicable to the MLG that mounts any Goodyear, Michelin, or Michelin Improved tires.

32-11-104 Discard of the Main Landing Gear (MLG) Assembly Side Stay Fitting Shaft

DS98414 FC 98414 FC

LIFE Canadair P/N 601R10237-1 Note: These lives are applicable to the MLG that mounts any Goodyear, Michelin, or Michelin Improved tires.

32-11-105 Discard of the Main Landing Gear (MLG) Assembly Uplock Assembly

DS

72600 FC 72600 FC


32-11-106a Discard of the Main Landing Gear (MLG) Assembly Cylinder -Shock Strut Piston - Shock Strut

DS120000 FC 120000 FC

LIFE Vendor P/N 17104 Note: These lives are applicable to the MLG that mounts any Goodyear, Michelin, or Michelin Improved tires.

32-11-106b Discard of the Main Landing Gear (MLG) Assembly Cylinder -Shock Strut Piston - Shock Strut

DS120000 FC 120000 FC


32-11-107 Discard of the Main Landing Gear (MLG) Assembly Shock Strut Pin

DS

120000 FC 120000 FC

LIFE Vendor P/N 17207-1 Note: P/Ns 17134-1 / -3 and 17144-1 removed from service as per Airworthiness Directive CF-96-12 R1. Note: These lives are applicable to the MLG that mounts any Goodyear, Michelin, or Michelin Improved tires.




32-11-108a Discard of the Main Landing Gear (MLG) Assembly Trailing Arm

DS

63869 FC 63869 FC


32-11-108b Discard of the Main Landing Gear (MLG) Assembly Trailing Arm

DS

63869 FC 63869 FC


32-11-108c Discard of the Main Landing Gear (MLG) Assembly Trailing Arm

DS

63869 FC 63869 FC


32-11-108d Discard of the Main Landing Gear (MLG) Assembly Trailing Arm

DS

120000 FC 120000 FC


32-11-110a Discard of the Main Landing Gear (MLG) Assembly Main Fitting

DS

66143 FC 66143 FC

LIFE Canadair P/N 601R85001-3 and Vendor P/N 17064-101 NOTE:1. P/Ns 601R85001−3 and −4 are removedfrom service by Airworthiness DirectiveCF−2004−18R1.

32-11-110b Discard of the Main Landing Gear (MLG) Assembly Main Fitting

DS

66143 FC 66143 FC


32-11-110c Discard of the Main Landing Gear (MLG) Assembly Main Fitting

DS

66143 FC 66143 FC


32-11-110d Discard of the Main Landing Gear (MLG) Assembly Main Fitting

DS

66143 FC 66143 FC





32-11-110e Discard of the Main Landing Gear (MLG) Assembly Main Fitting

DS

66143 FC 66143 FC

LIFE Canadair P/N 601R85001-81 and Vendor P/N 17064-105 Note: 2. P/Ns 601R85001−81 and −82 areremoved from service by AirworthinessDirective CF−2003−09R1.

32-11-110f Discard of the Main Landing Gear (MLG) Assembly Main Fitting

DS

66143 FC 66143 FC

LIFE Canadair P/N 601R85001-82 and Vendor P/N 17064-106 Note: 2. P/Ns 601R85001−81 and −82 areremoved from service by AirworthinessDirective CF−2003−09R1.

32-11-110g Discard of the Main Landing Gear (MLG) Assembly Main Fitting

DS

120000 FC 120000 FC


32-11-110h Discard of the Main Landing Gear (MLG) Assembly Main Fitting

DS

120000 FC 120000 FC


32-11-111 Discard of the Main Landing Gear (MLG) Assembly Axle DS120000 FC 120000 FC


32-11-112 Discard of the Main Landing Gear (MLG) Assembly Side Stay Actuator Cylinder

DS120000 FC 120000 FC

LIFE Vendor P/N 17027-8 Note: These lives are applicableto the MLG that mounts any Goodyear, Michelin, or Michelin Improved tires.

32-11-113 Discard of the Main Landing Gear (MLG) Assembly Side Stay Actuator Piston

DS113355 FC 113355 FC


32-11-114 Discard of the Main Landing Gear (MLG) Assembly Side Stay Actuator Rod End

DS113355 FC 113355 FC

LIFE Vendor P/N 17028-3 Note: These lives are applicableto the MLG that mounts any Goodyear, Michelin, or Michelin Improved tires.

32-11-116 Discard of the Main Landing Gear (MLG) Assembly Pivot Pin DS120000 FC 120000 FC


32-11-117 Discard of the Main Landing Gear (MLG) Assembly Side Stay Actuator Pin

DS120000 FC 120000 FC


32-11-118 Discard of the Main Landing Gear (MLG) Assembly Pintle Pin

DS64607 FC 64607 FC





32-21-101a Discard of the Nose Landing Gear (NLG) Assembly DS

132616 FC 132616 FC

LIFE Canadair P/N 601R85002-1 and Vendor P/N 16040-101 Note: These lives are applicable to the NLG that mounts any Goodyear, Michelin, or Michelin Improved tires.

32-21-101b Discard of the Nose Landing Gear (NLG) Assembly DS

132616 FC 132616 FC


32-21-101c Discard of the Nose Landing Gear (NLG) Assembly DS

132616 FC 132616 FC


32-21-101d Discard of the Nose Landing Gear (NLG) Assembly DS

132616 FC 132616 FC


32-21-101e Discard of the Nose Landing Gear (NLG) Assembly DS

132616 FC 132616 FC


32-21-101f Discard of the Nose Landing Gear (NLG) Assembly DS

132616 FC 132616 FC


32-21-101g Discard of the Nose Landing Gear (NLG) Assembly DS

132616 FC 132616 FC


32-21-101h Discard of the Nose Landing Gear (NLG) Assembly DS

132616 FC 132616 FC


32-21-101k Discard of the Nose Landing Gear (NLG) Assembly DS

132616 FC 132616 FC


32-21-102a Discard of the Nose Landing Gear (NLG) Assembly Uplock Assembly

DS

106667 FC 106667 FC


32-21-102b Discard of the Nose Landing Gear (NLG) Assembly Uplock Assembly

DS

106667 FC 106667 FC





32-21-103 Discard of the Nose Landing Gear (NLG) Drag Brace DS

22265 FC 22265 FC


32-21-104a Discard of the Nose Landing Gear (NLG) Assembly Drag Brace

DS

57897 FC 57897 FC


32-21-104b Discard of the Nose Landing Gear (NLG) Assembly Drag Brace

DS

57897 FC 57897 FC


34-11-01 Discard of the Pitot-Static and Temperature Sensing System Probe - Pitot - Static

DS9600 FH 9600 FH

LIFE Note: Life Limit applicable to aircraft Post SB 601R-34-080 (RVSM) Vendor P/N 0856KV9 and 0856KV10

49-20-01 Discard APU Compressor Rotor DS100000 AH 100000 AH

LIFE Effective for APU's that are on Life Limited Parts Program. P/N: 3822281-1

49-20-02 Discard APU Turbine Rotor DS

10000 AH 10000 AH

LIFE Effective for APU's that are on Life Limited Parts Program. P/N: 3842132-1 P/N: 3842132-2, SB GTCP36-49-7443

52-11-02 Discard of the Passenger Door Torsion Spring - Lock Mechanism

DS 2300 FC 2300 FC LIFE Canadair P/N 601R318911-1

52-11-03 Discard of the Passenger Door Spring - Outer Handle DS

1000 FC 1000 FC

LIFE Note: For P/N LC085H8 Detent Assembly Springs with more than 1000 flight cycles time in service, discard within the next 100 flight hours, and every 1000 flight cycles thereafter. Vendor P/N LC085H8

52-11-04 Discard of the Passenger Door Bushing - Upper Latch Fitting DS 4500 FH 4500 FH LIFE Vendor P/N NAS537B16P034W and NAS76A16-011

52-11-08 Discard of the Passenger Door Motor - Passenger Door DS 50000 FC 50000 FC LIFE Canadair P/N 601R94556-3 and Vendor P/N 2R5206B

52-11-101a Detailed Visual Inspection of the Passenger Door - Internal and External Structure

DVI 40000 FC 40000 FC EFFECTIVITY:Pre−Modsum TC601R13193

52-11-101b Detailed Visual Inspection of the Passenger Door - Internal and External Structure

SDI 40000 FC 40000 FC EFFECTIVITY:Pre−Modsum TC601R13193

52-11-102 Passenger door − brackets, fittings and supportstructure


52-11-104a Detailed Visual Inspection of the Phase IV Passenger Door - Internal and External

DVI 40000 FC 22527 FC EFFECTIVITY: Post-Modsum TC601R13193

52-11-104b Detailed Visual Inspection of the Phase IV Passenger Door - Internal and External

SDI 40000 FC 22527 FC EFFECTIVITY: Post-Modsum TC601R13193




52-11-105 Phase IV Passenger door − brackets, fittingsand support structure


52-11-131 Passenger door − piano hinge half on door side DVI

5700 FC 5700 FC

PHASE−IN:Do the Threshold (initial) inspection as follows:1. For aircraft with 3200 Flight Cycles (FC) orless, accomplish before 5700 FC.2. For aircraft with 3200 FC or more, accomplishwithin 2500 FC.NOTE:Subject to TC AD action.

52-21-102 Detailed Visual Inspection of the Overwing Emergency Exit Door

DVI 9000 FC 1000 FC EFFECTIVITY: Pre-Modsum TC601R25121

52-21-104 Detailed Visual Inspection of the Overwing Emergency Exit Door

DVI 40000 FC 9000 FC EFFECTIVITY: Post-Modsum TC601R25121 and Pre-Modsum TC601R25160

52-21-105 Detailed Visual Inspection of the Overwing Emergency Exit Door Casting


52-22-102 Detailed Visual Inspection of the Crew Escape Hatch Pin Fittings, Stop Brackets, and Support Structure

DVI 20538 FC 20538 FC

52-22-103 Detailed Visual Inspection of the Crew Escape Hatch Pin Fittings, Stop Brackets, and Support Structure


52-31-102 Detailed Visual Inspection of the Cargo Door Structure DVI 40000 FC 40000 FC 52-41-102 Detailed Visual Inspection of the Service Door Fittings and

Back Up StructureDVI 40000 FC 34000 FC

52-42-103 Detailed Visual Inspection of the Avionics Compartment Door Fittings and Back Up Structure

DVI 40000 FC 40000 FC

53-11-101-1 Detailed Visual Inspection of the Nose Landing Gear (NLG) and Drag Strut, Trunnion Fittings, and Local Beam Structure

DVI

27000 FC 25250 FC


53-11-101-2 Detailed Visual Inspection of the Nose Landing Gear (NLG) and Drag Strut, Trunnion Fittings, and Local Beam Structure

DVI

18000 FC 16800 FC

EFFECTIVITY: Post-Modsum TC601R15827

53-11-102 Detailed Visual Inspection of the Nose Landing Gear (NLG) Wheel Well, Vertical Stiffener Lower Attachment

DVI 40000 FC 40000 FC

53-11-103 Detailed Visual Inspection of the Nose Landing Gear (NLG) Wheel Well Upper Cap Angles Between FS 202.75 and FS 235.0

DVI40000 FC 40000 FC

53-11-104 Detailed Visual Inspection of the Flight Compartment Floor Connection to the Forward Pressure Bulkhead at FS 202.75

DVI40000 FC 40000 FC

53-11-106 Detailed Visual Inspection of the Forward Pressure Bulkhead DVI 14874 FC 14874 FC TR 2B-2118 EFFECTIVITY: Pre-Modsum TC601R16895




53-11-108-1 Detailed Visual Inspection of the Frame FS 235.0 Lower Sector Web and Caps

DVI

40000 FC 24700 FC

Pre-Modsum TC601R15827

53-11-108-2 Detailed Visual Inspection of the Frame FS 235.0 Lower Sector Web and Caps

DVI

40000 FC 16467 FC

Post-Modsum TC601R15827

53-11-110 Detailed Visual Inspection of the Flight Crew Escape Hatch Surround Structure and Stop Fittings

DVI 12557 FC 12028 FC

53-11-112 Detailed Visual Inspection of the Fuselage Skin FS 212.0 to FS 280.0 at Cockpit Floor Level

DVI 40000 FC 18868 FC

53-11-121 Special Detailed Inspection of the Cockpit Side Window Aft End Post (Framing Member) at Bulkhead FS 280.0

SDI 40000 FC 10500 FC

53-11-122a Windshield center post and bulkhead aft post atFS202.75

SDI

24705 FC 7779 FC

EFFECTIVITY:Pre−Modsum TC601R15021ANDPre−Modsum TC601R16895PHASE−IN:For aircraft that have exceeded the reducedthreshold, do the initial threshold inspection asfollows:1. For aircraft with 21705 FC or less, inspectbefore 24705 FC.2. For aircraft with 21706 FC to 24705 FC,inspect within 3000 FC, but not later than26705 FC. 3. For aircraft with 24706 FC or more, inspectwithin 2000 FC.NOTE:Subject to TC AD action.




53-11-122b Windshield center post and bulkhead aft post atFS202.75

DVI

24705 FC 7779 FC

EFFECTIVITY:Pre−Modsum TC601R15021ANDPre−Modsum TC601R16895PHASE−IN:For aircraft that have exceeded the reducedthreshold, do the initial threshold inspection asfollows:1. For aircraft with 21705 FC or less, inspectbefore 24705 FC.2. For aircraft with 21706 FC to 24705 FC,inspect within 3000 FC, but not later than26705 FC. 3. For aircraft with 24706 FC or more, inspectwithin 2000 FC.NOTE:Subject to TC AD action.

53-11-123 Special Detailed Inspection of the Windshield Side Post Upper and Lower Joints to Sills and Fuselage Fittings

SDI 40000 FC 10849 FC

53-11-124-1 Detailed Visual Inspection of the Nose Landing Gear (NLG) Wheel Well Skin Cutout at FS 235.0 and BL 6.0

DVI 16448 FC 16448 FC Pre-Modsum TC601R15827

53-11-124-2 Detailed Visual Inspection of the Nose Landing Gear (NLG) Wheel Well Skin Cutout at FS 235.0 and BL 6.0

DVI 10965 FC 10965 FC Post-Modsum TC601R15827

53-11-126 Detailed Visual Inspection of the Flitefone VI Antenna Cutout at FS 250.0, Str 26

DVI 40000 FC 12377 FC Note 3

53-11-127a Special Detailed Inspection of the Windshield Center Post and Bulkhead Aft Post at FS 202.75

SDI 24705 FC 7779 FC TR 2B-2122 - EFFECTIVITY: Post-Modsum TC601R15021

53-11-127b Detailed Visual Inspection of the Windshield Center Post and Bulkhead Aft Post at FS 202.75

DVI 24705 FC 7779 FC TR 2B-2122 - EFFECTIVITY: Post-Modsum TC601R15021

53-11-128 Detailed Visual Inspection of the Forward Pressure Bulkhead DVI 40000 FC 18400 FC TR 2B-2122...... EFFECTIVITY: Post-Modsum TC601R16895

53-11-129a Special Detailed Inspection of the Windshield Center Post and Bulkhead Aft Post at FS202.75

SDI 40000 FC 8047 FC TR 2B-2122 - EFFECTIVITY: Post-Modsum TC601R15021 and Post-Modsum TC601R16895

53-11-129b Detailed Visual Inspection of the Windshield Center Post and Bulkhead Aft Post at FS202.75

DVI 40000 FC 8047 FC TR 2B-2122 - EFFECTIVITY: Post-Modsum TC601R15021 and Post-Modsum TC601R16895

53-11-130a Special Detailed Inspection of the Windshield Center Post and Bulkhead Aft Post at FS202.75

SDI 40000 FC 10847 FC TR 2B-2122 - EFFECTIVITY: Pre-Modsum TC601R15021 and Post-Modsum TC601R16895

53-11-130b Detailed Visual Inspection of the Windshield Center Post and Bulkhead Aft Post at FS202.75

DVI 40000 FC 10847 FC TR 2B-2122 - EFFECTIVITY: Pre-Modsum TC601R15021 and Post-Modsum TC601R16895

53-21-101 Detailed Visual Inspection of the Passenger Door Cutout Upper and Lower Sills

DVI 20283 FC 16750 FC

53-21-102 Detailed Visual Inspection of the Passenger Door Cutout Frames and Internal Back-Up Structure

DVI 40000 FC 20850 FC NOTE: Subject to TC AD action




53-21-103 Detailed Visual Inspection of the Passenger Door Fittings On Fuselage


53-21-108 Detailed Visual Inspection of the Service Door Cutout Support Frames, Sills, and Back-Up Structure

DVI 13153 FC 13153 FC

53-21-110 Detailed Visual Inspection of the Avionics Compartment Door Cutout Surrounding Structure

DVI 39292 FC 18514 FC

53-21-115 Detailed Visual Inspection of the Fuselage Structure from FS 280.0 to FS 409.0 Above the Floor


53-21-118 Detailed Visual Inspection of the Potable Water Servicing Door Cutout and Internal Structure


53-21-119 Detailed Visual Inspection of the Rear Lavatory Servicing Door Cutout and Internal Structure

DVI 26195 FC 12343 FC

53-21-125 Detailed Visual Inspection of the Circumferential Fuselage Splice at FS 280.0

DVI 40000 FC 6604 FC

53-21-126 Detailed Visual Inspection of the Phase IV Passenger Door Cutout Upper and Lower Sills


53-21-127 Detailed Visual Inspection of the 'Phase IV Passenger Door Cutout Frames and Internal Back-Up Structure

DVI 40000 FC 9833 FC EFFECTIVITY: Post-Modsum TC601R13193 Note: Subject to TC AD action.

53-21-128 Detailed Visual Inspection of the Phase IV Passenger Door Fittings On Fuselage


53-21-129 Passenger door − piano hinge half on fuselageside

DVI

5700 FC 5700 FC

PHASE−IN:Do the Threshold (initial) inspection as follows:1. For aircraft with 3200 Flight Cycles (FC) orless, accomplish before 5700 FC.2. For aircraft with 3200 FC or more, accomplishwithin 2500 FC.NOTE:Subject to TC AD action.

53-41-101 Detailed Visual Inspection of the ADF Antenna and DME Antenna Cutouts

DVI 32000 FC 8409 FC

53-41-103 Detailed Visual Inspection of the Emergency Light Cutout In the Exterior Side Panel, FS 409.0 to FS 409.0 + 128

DVI 40000 FC 40000 FC

53-41-104 Detailed Visual Inspection of the Forward Keel Beam Bayonet Fittings

DVI 40000 FC 13530 FC

53-41-107 Detailed Visual Inspection of the VHF Antenna Cutout at FS 455.8, Str 0

DVI 40000 FC 12030 FC

53-41-108 Detailed Visual Inspection of the Skin at Str 6 and Frames FS 424.0, FS 449.0, FS 473.0 and FS 513.0

DVI 40000 FC 23195 FC

53-41-109 Special Detailed Inspection of the Longitudinal Str 6 Splice, FS 409.0 + 80 to FS 559.0 + 48

SDI 18744 FC 3563 FC

53-41-110 Special Detailed Inspection of the Longitudinal Str 6 Splice Butt Strap at Str 6, FS 409.0 to FS 559.0 + 112

SDI 38398 FC 38398 FC




53-41-111-1 Detailed Visual Inspection of the Skin Panel at Machined Frames, FS 409.0 + 128 to FS 559.0

DVI

40000 FC 13297 FC


53-41-111-2 Detailed Visual Inspection of the Skin Panel at Machined Frames, FS 409.0 + 128 to FS 559.0

DVI

40000 FC 8865 FC


53-41-112 Detailed Visual Inspection of the Emergency Light Cutouts In Side Skin Panel, FS 409.0 + 128 to FS 559.0

DVI 40000 FC 40000 FC

53-41-116 Detailed Visual Inspection of the Vertical Beams on Frame FS 409.0 + 128 and FS 559.0

DVI

14906 FC 12823 FC

Note: 1). For aircraft that have exceeded the reduced threshold/repeat interval, comply with the threshold (initial) inspection as follows: A). For aircraft with 10906 FC or less, inspect prior to exceeding 14906 FC. B). For aircraft with more than 10906 FC, but no more than 14906 FC, inspect within the next 4000 FCbut not exceeding 17906 FC. C). For aircraft with more than 14906 FC, but no more than 20406 FC, inspect within the next 3000 FC but not exceeding 21906 FC. D). For aircraft with more than 20406 FC, inspect within the next 1500 FC. 2). Phase In time of Airworthiness Directive (AD) will take Precedence to the above.

53-41-119 Special Detailed Inspection of the Frame FS 409.0 + 128 andFrame FS 559.0 Local to the Floor Level

SDI

27855 FC 13273 FC

PHASE−IN:Do the Threshold (initial) inspection as follows:1. For aircraft with 22855 Flight Cycles (FC) orless, accomplish before 27855 FC.2. For aircraft with 22856 FC to 27855 FC, accomplish within 5000 FC, but not later than 31855 FC. 3. For aircraft with 27856 FC or more, accomplish within 4000 FC. NOTE:Subject to TC AD action.

53-41-120 Special Detailed Inspection of the Frame FS 559.0 Splice at Str 0

SDI 30675 FC 6127 FC

53-41-124 Detailed Visual Inspection of the Bulkhead Webs at Frame FS 559.0 and at Frame FS 409.0 + 128

DVI 18325 FC 18325 FC

53-41-125 Detailed Visual Inspection of the Overwing Emergency Exit, Door Cutout, Frames, and Internal Back-Up Structure

DVI40000 FC 40000 FC




53-41-126 Special Detailed Inspection of the Cabin Window Surround Structure

SDI

10047 FC 10047 FC

EFFECTIVITY: Pre-Modsum TC601R12201 Note: SSI 53-41-126 is applicable to the Pre-Modsum TC601R12201 aircraft and includes both Pre and Post SB 601R-53-025 incorporation. Note: For aircraft that have exceeded the threshold period of 10047 flights and for aircraft that have accumulated more than 9697 flights, a phase in period of 1350 flights is allowed from Nov 08/98. The second inspection shall occur at 20094 flights since production delivery and all subsequent repeat inspections shall remain at the established 10047 flight intervals. Note: For aircraft that have incorporated the SB 601R-53-025, at the option of the operator, the threshold inspection shall be 10047 flights from the time of incorporation of the SB.

53-41-127 Special Detailed Inspection of the Circumferential Fuselage Joint at Frame FS 559.0

SDI 21932 FC 9228 FC

53-41-128 Special Detailed Inspection of the Circumferential Fuselage Joint at FS 409.0 + 128

SDI 21932 FC 9228 FC

53-41-132-1 Special Detailed Inspection of the Frame FS 424.0 and FS 513.0 Inner and Outer Caps from Str 14 to WL73.0

SDI40000 FC 7639 FC


53-41-132-2 Special Detailed Inspection of the Frame FS 424.0 and FS 513.0 Inner and Outer Caps from Str 14 to WL73.0

SDI40000 FC 5093 FC


53-41-133-1 Detailed Visual Inspection of the Frame FS 424.0 Wing Attachment Lugs

DVI 40000 FC 8108 FC EFFECTIVITY: Pre-Modsum TC601R15827

53-41-133-2 Detailed Visual Inspection of the Frame FS 424.0 Wing Attachment Lugs


53-41-134 Detailed Visual Inspection of the Frame FS 449.85 Inner Cap from Str 8 to Str 11

DVI 40000 FC 8037 FC

53-41-138-1 Detailed Visual Inspection of the Frame FS 473.15 Wing Attachment Lug

DVI40000 FC 6374 FC


53-41-138-2 Detailed Visual Inspection of the Frame FS 473.15 Wing Attachment Lug

DVI40000 FC 4249 FC


53-41-139 Detailed Visual Inspection of the Frames FS 424.0, FS 473.0 and FS 513.0

DVI 40000 FC 40000 FC

53-41-141 Special Detailed Inspection of the Frame FS 513.0 Under Floor BL 0.0 Splice

SDI 11387 FC 5093 FC EFFECTIVITY: Pre-Modsum TC601R14160 and Pre-SB 601R-29-020




53-41-142-1 Detailed Visual Inspection of the Frame FS 513.0, BL 13.0, Wing Attachment Fitting

DVI38773 FC 6374 FC


53-41-142-2 Detailed Visual Inspection of the Frame FS 513.0, BL 13.0, Wing Attachment Fitting

DVI25849 FC 4249 FC


53-41-145 Special Detailed Inspection of the Overwing Floor Support Beam at FS 460.0

SDI 40000 FC 2857 FC

53-41-146 Special Detailed Inspection of the Pressure Floor Skin Access Panel Cut-Outs

SDI 40000 FC 28460 FC

53-41-149 Detailed Visual Inspection of the Pressure Floor Skin DVI

10000 FC 10000 FC

Note: For aircraft that exceeded the reduced threshold/repeat interval, comply with the threshold (initial) inspection as follows: 1). For aircraft with 8000 FC or less, inspect prior to exceeding 10000 FC. 2). For aircraft with more than 8000 FC, but lessthan 10000 FC, inspect within the next 2000 FC. 3). For aircraft with 10000 FC or more, but less than 15000 FC, inspect within the next 1500 FC. 4). For aircraft with 15000 FC or more but less than 17325 FC, inspect within the next 1000 FC. 5). For aircraft with 17325 FC or more, but less than 18325 FC, inspect prior to exceeding 18325 FC. 6). For aircraft that have completed the inspection at 18325 FC, inspect at the repeat interval above. Note: Phase in time of an Airworthiness Directive (AD) will take precedence to the above.

53-41-150 Detailed Visual Inspection of the Pressure Floor Support Beams

DVI 37070 FC 37070 FC

53-41-155 Detailed Visual Inspection of the Pressure Floor Sill Member FS 409.0 + 128 to FS 559.0

DVI 40000 FC 5324 FC

53-41-156 Detailed Visual Inspection of the Pressure Floor Intercostals DVI 40000 FC 10403 FC

53-41-157 Detailed Visual Inspection of the Frame Attachment to Sill and Longeron

DVI 40000 FC 38752 FC

53-41-158 Detailed Visual Inspection of the Underfloor Longeron Assembly - FS 409.0 + 128

DVI 40000 FC 40000 FC




53-41-159-1 Detailed Visual Inspection of the Longeron at FS 424.0 DVI

24032 FC 4547 FC

EFFECTIVITY: Pre-Modsum TC601R15827 PHASE-IN: Do the Threshold (initial inspection as follows: 1. For aircraft with 21032 Flight Cycles (FC) or less, accomplish before 24032 FC. 2. For aircraft wiht 21033 FC to 24032 FC, accomplish wihtin 3000 FC, but not later than 26032 FC. 3. For aircraft with 24033 FC to 26032 FC, accomlish within 2000 FC , but not later than 27032 FC. 4. For aircraft with 26033 FC or more, accomplish within 1000 FC. NOTE: Subject to TC AD action

53-41-159-2 Detailed Visual Inspection of the Longeron at FS 424.0 DVI

16021 FC 3031 FC

EFFECTIVITY: Post-Modsum TC601R15827 PHASE-IN: Do the Threshold (initial inspection as follows: 1. For aircraft with 21032 Flight Cycles (FC) or less, accomplish before 24032 FC. 2. For aircraft wiht 21033 FC to 24032 FC, accomplish wihtin 3000 FC, but not later than 26032 FC. 3. For aircraft with 24033 FC to 26032 FC, accomlish within 2000 FC , but not later than 27032 FC. 4. For aircraft with 26033 FC or more, accomplish within 1000 FC. NOTE: Subject to TC AD action

53-41-161-1 Special Detailed Inspection of the Underfloor, BL45.0, Longeron Lower Flange

SDI40000 FC 1702 FC


53-41-161-2 Special Detailed Inspection of the Underfloor, BL45.0, Longeron Lower Flange

SDI40000 FC 1135 FC


53-41-162 Detailed Visual Inspection of the Underfloor, BL45.0, Longeron Web

DVI 40000 FC 40000 FC

53-41-163 Detailed Visual Inspection of the Underfloor, BL45.0, Longeron Upper Flange


53-41-165 Detailed Visual Inspection of the Upper Skin Panel FS 559.0 to FS 559.0 + 112

DVI 40000 FC 3717 FC

53-41-166 Detailed Visual Inspection of the Side Skin Panel FS 559.0 to FS 559.0 + 112

DVI 40000 FC 40000 FC

53-41-168 Detailed Visual Inspection of the Pressure Floor Sill Web from FS 409.0 + 128 to FS 559.0

DVI 40000 FC 8260 FC




53-41-171 Detailed Visual Inspection of the Oxygen Indicator Cutout at FS 409.0 + 80, Str 24

DVI 40000 FC 6761 FC Note 3

53-41-176 Detailed Visual Inspection of the GPS Antenna Cutouts (Dual and Single Antenna Installations) Between FS 409.0 + 32 and FS 409.0 + 48 and Str 1L and 1R

DVI40000 FC 5500 FC

Note 3

53-41-177 Detailed Visual Inspection of the Keel Beam Cutout at FS 409.0 + 128

DVI

4500 FC 450 FC

EFFECTIVITY: Post-Modsum TC601R14465 and Post SB 601R-53-047. Note: This SSI is Superseded by SSI 53-41-184 and SSI 53-41-185 if Mod Sum TC601R14589 or SB 601R-53-050 is incorporated before 5400 FC from incorporation of SB 601R-53-047 or Mod Sum TC601R14465. The incorporation limit can be extended from 5400 to 7000 FC if the special inspection from Appendix C of SB 601R-53-050 is completed when SB 601R-53-050 is incorporated. The threshold inspection interval for SSI 53-41-177 starts from the incorporation of SB 601R-53-047 or Modsum TC601R14465.


DVI

23530 FC 23530 FC

EFFECTIVITY: Pos- Modsum TC601R25125, TC601R25126, TC601R25127. Note: SSI 53-41-179 applies to aircraft that incorporates all three Mod Sums. This SSI 53-41-179 is superseded by SSI 53-41-180 is SB 601R-53-050 is incorporated before 8000 FC from aircraft delivery.

53-41-180 Detailed Visual Inspection of the Strap Modification to the FS 409.0 + 128 Bulkhead

DVI

40000 FC 40000 FC

Post-Modsums TC601R25125, TC601R25126, and TC601R25127 with reinforcing strap. Note: This SSI 53-41-180 applies to aircraft which have incorporated all three Mod Sums and have either: 1). IncorporatedMod Sum TC601R25128 before aircraft delivery, or 2) Incorporated SB 601R-53-050 before 8000 FC from aircraft delivery. The threshold inspection interval for SSI 53-41-180 starts from aircraft delivery.

53-41-182 Special Detailed Inspection of the Frame FS 513.0 Under Floor BL 0.0 Splice

SDI 40000 FC 38253 FC EFFECTIVITY: Post-Modsum TC601R14160 and Post SB 601R-29-020

53-41-183 Special Detailed Inspection of the Cabin Window Surround Structure

SDI

21113 FC 10047 FC

EFFECTIVITY: Post-Modsum TC601R12201. Note: AWL 53-41-183 is not applicable to SB 601R-53-025 incorporation. Refer to AWL 53-41-126 for Pre or Post SB 601R-53-025 incorporation.




53-41-184 Special Detailed Inspection of the Strap Modification to the FS 409.0 + 128 Bulkhead

SDI

40000 FC 40000 FC

EFFECTIVITY: Post−Modsum TC601R14589 or Post SB 601R−53−050. Note: SSI 53−41−184 applies to aircraft which have not incorporated TC601R25125, TC601R25126, and TC601R25127 and have satisfied any one of the following conditions: 1). Incorporated SB 601R−53−050 within 5400 FC from the incorporation of SB 601R−53−047 or Mod Sum TC601R14465. 2). Incorporated SB 601R−53−050 within 7000 FC from the incorporation of SB 601R−53−047 or Mod Sum TC601R14465, and received the special inspection from Appendix C of SB 601R−53−050 when SB 601R−53−050 was incorporated. 3). Incorporated SB 601R−53−050 within 8000 FC from incorporation of SB 601R−53−046, REO 601R−53−31−012 (and deviations), REO 601R−53−31−019 or Air Canada drawing 53−10002. 4). Incorporation of SB 601R−53−050 within 20000 FC from the incorporation of SB 601R−53−046, REO 601R−53−31−012 (and its deviations), REO 601R−53−31−019 or Air Canada drawing 53−10002, and received the special inspection from Appendix C of SB 601R−53−050 when SB 601R−53−050 was incorporated......Compliance with AWL 53−41−184




53-41-185 Detailed Visual Inspection of the Strap Modification to the FS 409.0 + 128 Bulkhead

DVI

40000 FC 11860 FC

EFFECTIVITY: Post−Modsum TC601R14589 or Post SB 601R−53−050. Note: SSI 53−41−184 applies to aircraft which have not incorporated TC601R25125, TC601R25126, and TC601R25127 and have satisfied any one of the following conditions: 1). Incorporated SB 601R−53−050 within 5400 FC from the incorporation of SB 601R−53−047 or Mod Sum TC601R14465. 2). Incorporated SB 601R−53−050 within 7000 FC from the incorporation of SB 601R−53−047 or Mod Sum TC601R14465, and received the special inspection from Appendix C of SB 601R−53−050 when SB 601R−53−050 was incorporated. 3). Incorporated SB 601R−53−050 within 8000 FC from incorporation of SB 601R−53−046, REO 601R−53−31−012 (and deviations), REO 601R−53−31−019 or Air Canada drawing 53−10002. 4). Incorporation of SB 601R−53−050 within 20000 FC from the incorporation of SB 601R−53−046, REO 601R−53−31−012 (and its deviations), REO 601R−53−31−019 or Air Canada drawing 53−10002, and received the special inspection from Appendix C of SB 601R−53−050 when SB 601R−53−050 was incorporated......Compliance with AWL 53−41−184


DVI

13358 FC 2049 FC

EFFECTIVITY: Post SB 601R−53−046, No CHQ A/C effective. Note: This SSI 53−41−184 and SSI 53−41−185 if Mod Sum TC601R14589 or SB 601R−53−050 is incorporated before 8000 FC from the incorporation of SB 601R−53−046. The incorporation limit can be extended from 8000 to 20000 FC if the special inspection from Appendix C of SB 601R−53−050 is completed when SB 601R−53−050 is incorporated. The threshold inspection interval for SSI 53−41−188 starts with the incorporation of SB 601R−53−046.




53-41-189 Special Detailed Inspection of the Keel Beam Cutout at FS 409 + 128

SDI

13358 FC 2049 FC

EFFECTIVITY: Post SB 601R-53-046. No CHQ A/C effective. Note: This SSI 53-41-189 is superseded by SSI 53-41-184 and SSI 53-41-185 if Mod Sum TC601R14589 or SB 601R-53-050 is incorporated before 8000 FC from the incorporation of SB 601R-53-046. The incorporation limit can be extended from 8000 to 20000 FC if the special inspection form Appendix C of SB 601R-53-050 is completed when SB 601R-53-050 is incorporated. The threshold inspection interval for SSI 53-41-189 starts with the incorporation of SB 601R-53-046.

53-41-190 Detailed Visual Inspection of the Strobe Light Cut-Outs at FS 409.0 + 24 to Local to STR 0 to STR 27

DVI 40000 FC 40000 FC EFFECTIVITY: Optional beacon light installation.

53-41-191 Special Detailed Inspection of the Frame 559 Inner Cap Between STR 2 and STR 9, LHS and RHS

SDI 40000 FC 34353 FC

53-41-192 Special Detailed Inspection of the Frame FS 409 + 128 Inner Cap Between STR 11L and STR 11R

SDI 40000 FC 40000 FC

53-41-193 Detailed Visual Inspection of the Internal Pressure Floor Skin, FS 409.00 + 128 to FS 559.00, Left Extremity of Floor to Right Extremity

DVI

10000 FC 10000 FC

EFFECTIVITY:Post−Modsum TC601R25208ORPost−Modsum TC601R25274ORPost−Modsum TC601R25336ORPost−Modsum TC601R25337

53-41-194 Pressure floor Post Retro Mods at FS460.00 andFS513.00, between LBL18.0 and RBL18.0

SDI

40000 FC 16185 FC

EFFECTIVITY:Post−Modsum TC601R25274ORPost−Modsum TC601R25336

53-41-195 Pressure floor Post Production Mods at FS460.00and FS513.00, between LBL18.0 and RBL18.0

SDI

40000 FC 16352 FC

EFFECTIVITY:Post−Modsum TC601R25208ORPost−Modsum TC601R25337

53-41-196 Special Detailed Inspection FS409.00+128 Vertical Beams at BL 0.0 and BL 18.0


53-41-197 Special Detailed Inspection FS409.00+128 Vertical Beams at BL 0.0 and BL 18.0


53-41-198 Detailed Visual Inspection FS409.00+128 Splice Angles at STR 21L and STR 21R

DVI 40000 FC 32703 FC EFFECTIVITY: Post-Modsum TC601R25328 or Post-Modsum TC601R25334




53-41-199 Special Detailed Inspection of the FS 409.0 + 128 Vertical Posts at BL 0.0 and BL 18.0 Left and Right Local to WL 69.0

SDI

18156 FC 4845 FC

TR 2B−2123 PHASE IN: Do the Threshold (initial) inspections as follows: 1). For aircraft with 14156 FC or less, accomplish before 18156 FC. 2). For aircraft with 14157 FC to 18156 FC, accomplish within 4000 FC, but not later than 21156 FC. 3). For aircraft with 18157 to 21156 FC, accomplish within 2500 FC, but not later than 23656 FC. 4). For aircraft with 21157 to 23656 FC, accomplish within 2500 FC, but not later than 25156 FC. 5). For aircraft with 23657 FC or more, accomplish within 1500 FC. Note: Subject to TC AD action.

53-41-200 Detailed Visual Inspection of the FS 409.0 + 128 Frame Cap Aft and Forward Splice Angles at Str 21 Left and Right

DVI

26727 FC 8149 FC

TR 2B−2123 PHASE IN: Do the Threshold (initial) inspections as follows: 1). For aircraft with 23727 FC or less, accomplish before 26727 FC. 2). For aircraft with 23728 to 26727 FC, accomplish within 3000 FC, but not later than 28727 FC. 5). For aircraft with 26728 FC or more, accomplish within 2000 FC. Note: Subject to TC AD action.

53-41-201 Special Detailed Inspection of the FS 559.0 Pressure Bulkhead Web and Cap Angle Local to BL 9.0 and BL 18.0 Left and Right

SDI

16926 FC 3193 FC

TR 2B−2123 PHASE IN: Do the Threshold (initial) inspections as follows: 1). For aircraft with 12926 FC or less, accomplish before 16926 FC. 2). For aircraft with 12927 to 16926 FC, accomplish within 4000 FC, but not later than 19926 FC. 3). For aircraft with 16927 to 19926 FC, accomplish within 3000 FC, but not later than 22426 FC. 4). For aircraft with 19927 to 22426 FC, accomplish within 2500 FC, but not later than 23926 FC. 5). For aircraft with 22427 FC or more, accomplish within 1500 FC. Note: Subject to TC AD action.

53-61-101 Detailed Visual Inspection of the Rear Pressure Bulkhead Vertical Stiffeners and Web

DVI 20000 FC 6215 FC

53-61-104 Detailed Visual Inspection of the Longeron to Str 1 Splice at Frame FS 718.0

DVI 40000 FC 40000 FC

53-61-105 Detailed Visual Inspection of the Rear Pressure Bulkhead Frame Cap Local to Str 12L

DVI 40000 FC 5710 FC

53-61-106 Detailed Visual Inspection of the Rear Fuselage to Vertical Stabilizer Drag Angle at FS 755.0

DVI 40000 FC 26626 FC

53-61-108 Detailed Visual Inspection of the Floor Beam Attachments to Rear Pressure Bulkhead

DVI 40000 FC 20000 FC

53-61-109 Special Detailed Inspection of the Pylon to Fuselage Attachment Structure at Fuselage Frames FS 672.2 and FS 682.0

SDI40000 FC 1512 FC




53-61-110 Special Detailed Inspection of the Engine Support Beam Upper and Lower Cap Angles at FS 625.3, between RBL 36.2 and LBL 36.2

SDI34460 FC 12509 FC

EFFECTIVITY: Pre-Modsum TC601R15054 or Pre SB 601R-53-059 Rev A or later. Note: Airworthiness Directive issued.

53-61-111 Special Detailed Inspection of the Skin and Frame Splice at FS 672.2, Local to Str 6 and Str 7

SDI 35088 FC 16829 FC

53-61-112 Special Detailed Inspection of the Frame FS 625.3 Splice at Str 9 and Str 10

SDI 40000 FC 40000 FC

53-61-113 Detailed Visual Inspection of the Skin Panel Local Rear Pressure Bulkhead Str 7L to Str 7R

DVI 40000 FC 23577 FC

53-61-114 Special Detailed Inspection of the Engine Support Beam Aft Face

SDI40000 FC 6460 FC

EFFECTIVITY: Pre-Modsum TC601R15054 or Pre SB 601R-53-059 Rev A or later. Note: Airworthiness Directive issued.

53-61-140 Special Detailed Inspection of the Cargo Door Upper Sill SDI 40000 FC 40000 FC 53-61-141 Special Detailed Inspection of the Cargo Door Skin Cutout SDI

9249 FC 5291 FC

EFFECTIVITY: Pre−Modsum TC601R16421 or Pre−Modsum TC601R16422. Note: 1). For aircraft that have exceeded the reduced threshold and repeat interval, do the threshold inspection as follows: A). For aircraft with 5249 FC or less since entry into service, inspect before 9249 FC. B). For aircraft with 5250 to 9249 FC since entry into service, inspect within the next 4000 FC, but not later than 12249 FC. C). For aircraft with 9250 to 12249 FC since entry into service, inspect within the next 3000 FC, but not later than 14249 FC. D). For aircraft with 12250 to 14249 FC since entry into service, inspect within the next 2000 FC, but not later than 15249 FC. E). For aircraft with 14250 to 15249 FC since entry into service, inspect within the next 1000 FC, but not later than 15749 FC. F). For aircraft with 15250 FC ormore since entry into service, inspect within the next 500 FC. 2). Airworthiness Directive issued.

53-61-142 Special Detailed Inspection of the Engine Support Beam Cap Angle Area (Upper and Lower) at FS 640.0 and at 625.0 between RBL 36.2 and LBL 36.2

SDI

40000 FC 12095 FC

EFFECTIVITY: Post-Modsum TC601R15054 or Post-Modsum TC601R16135 or Post-Modsum TC601R16257 or Post SB 601R-53-059 Rev. A or later. Note: Airworthiness Directive issued.

53-61-143 Special Detailed Inspection of the Engine Support Beam Lower and Aft Web Access Holes Outboard of BL 36.2

SDI

22145 FC 11773 FC

EFFECTIVITY: Post-Modsum TC601R15054 or Post SB 601R-53-059 Rev. A or later. Note: 1). AWL 53-61-143 is superseded by AWL 53-61-146 for aircraft Post Modsum TC601R16299. 2). Airworthiness Directive issued.

53-61-145 Special Detailed Inspection of the Engine Support Beam, Lower and Aft Web Access Holes Outboard of BL 36.2 and Cap Angle Attachments at FS 625.3 and FS 640.0

SDI27040 FC 12509 FC

EFFECTIVITY: Post-Modsum TC601R16135 or Post-Modsum TC601R16394 or Post-Modsum TC601R16635




53-61-146 Special Detailed Inspection of the Engine Support Beam, Lower and Aft Web Access Holes Outboard of BL 36.2, Lower Web Splice and Cap Angle attachments at FS 625.3 and FS 640.0

SDI

27040 FC 10709 FC

EFFECTIVITY: Post-Modsum TC601R16257 or Post-Modsum TC601R16272 or Post-Modsum TC601R16299

53-61-147a Special Detailed Inspection of the FS 621.0 Rear Pressure Bulkhead Forward Face


53-61-147b Detailed Visual Inspection of the FS 621.0 Rear Pressure Bulkhead Forward Face


53-61-148 Special Detailed Inspection of the Engine Support Beam, Reinforcement to FS 640.0 Cap Angles for Baseline Structure already Repaired by GREO 601R-53-61-345

SDI10265 FC 10265 FC

EFFECTIVITY: Post-Modsum TC601R16420. Note: AWL 53-61-148 Supersedes GREO 601R-53-61-345 Inspection Requirements

53-61-149 Special Detailed Inspection of the Engine Support Beam, FS 640.0 Cap Angles, Preventive or Repair Modification


53-61-150 Special Detailed Inspection of the Baggage Door Skin Cutouts

SDI 14579 FC 14579 FC EFFECTIVITY: Post-Modsum TC601R16422 or Post SB 601R-53-070

53-61-151 Special Detailed Inspection of the Baggage Door Skin Cutouts


53-61-152a Special Detailed Inspection of the Engine Support Beam SDI 10265 FC 10265 FC EFFECTIVITY: Post SB 601R-53-07153-61-152b Detailed Visual Inspection of the Engine Support Beam DVI 10265 FC 10265 FC EFFECTIVITY: Post SB 601R-53-07153-61-153a Special Detailed Inspection of the Rear Pressure Bulkhead

Web Forward FaceSDI

12000 FC 4360 FC

Note 4. EFFECTIVITY: Pre-Modsum TC601R16159 or Pre-Modsum TC601R16430 Note: Compliance time to be in accordance with Airworthiness Directive. Per Note 4 Chautauqua Airlines chooses to perform the Visual Inspection Per AWL 53-61-153b.

53-61-153b Detailed Visual Inspection of the Rear Pressure Bulkhead Web forward Face

DVI

12000 FC 1085 FC

Note 4. EFFECTIVITY: Pre-Modsum TC601R16159 or Pre-Modsum TC601R16430 Note: Compliance time to be in accordance with Airworthiness Directive. Per Note 4 Chautauqua Airlines chooses to perform the Visual Inspection Per AWL 53-61-153b.

53-61-154 Detailed Visual Inspection of the Rear Pressure Bulkhead Web Forward Face


53-71-101 Detailed Visual Inspection of the Frame FS 755.0 Above WL 125.0

DVI 40000 FC 40000 FC

53-71-102 Detailed Visual Inspection of the Stringer Extension Attachment at VS 31.875% and VS 55.625%

DVI 40000 FC 40000 FC

53-71-103 Detailed Visual Inspection of the Vertical Stabilizer Rear Sparand Fuselage Frame at FS VS 67.5%

DVI 40000 FC 40000 FC

53-71-104 Detailed Visual Inspection of the Vertical Stabilizer Mid Spar and Fuselage Frame at FS VS 43.75%

DVI 40000 FC 40000 FC

53-71-105 Detailed Visual Inspection of the Vertical Stabilizer Front Spar Attachment Fittings at Frame FS 755.0

DVI 40000 FC 40000 FC




54-10-103 Special Detailed Inspection of the Engien Nacelle Aft Nose Cowl Bulkhead

SDI 40000 FC 40000 FC

54-10-104 Detailed Visual Inspection of the Engine Nacelle A4 Attachment Ring

DVI 40000 FC 40000 FC

54-10-105 Special Detailed Inspection of the Engine NacellePylon Trackand Support Fitting

SDI

29422 FC 5177 FC

PHASE−IN:Do the Threshold (initial) inspection as follows:1. For aircraft with 26422 Flight Cycles (FC) orless, accomplish before 29422 FC.2. For aircraft with 26423 FC to 29422 FC, accomplish within 3000 FC, but not later than 31422 FC. 3. For aircraft with 29423 FC or more, accomplish within2000 FC. NOTE: Subject to TC AD action

54-10-106 Special Detailed Inspection of the Engine Nacelle Pylon Track and Support Fitting

SDI 39480 FC 6042 FC EFFECTIVITY: Post-Modsum EB600-3283 and EB600-3526

54-51-101 Special Detailed Inspection of the Pylon Box Front Spar at FS 625.3

SDI 40000 FC 40000 FC

54-51-102 Detailed Visual Inspection of the Pylon Box Upper and Lower Skins from FS 672.0 to FS 682.0

DVI 40000 FC 16518 FC

54-51-103 Detailed Visual Inspection of the Pylon Box Canted Rib and Drag Braces

DVI 40000 FC 40000 FC

55-11-102 Detailed Visual Inspection of the Screwjack Attach Fittings On Horizontal Stabilizer Center Section Front Spar

DVI40000 FC 33564 FC

55-11-103 Detailed Visual Inspection of the Horizontal stabilizer Front Spar Splice at BL 6.0

DVI 40000 FC 40000 FC

55-11-105 Detailed Visual Inspection of the Horizontal Stabilizer Upper Surface Str 3

DVI 40000 FC 40000 FC

55-11-106 Detailed Visual Inspection of the Rear Spar Splice and Skin Structure - RBL 11.0 to LBL 11.0

DVI 40000 FC 40000 FC

55-11-110 Detailed Visual Inspection of the Horizontal Stabilizer BL 6.0 Rib

DVI 40000 FC 40000 FC

55-11-115 Detailed Visual Inspection of the Horizontal Stabilizer Elevator Hinges 1 and 1A Fittings - Mounted on Stabilizer

DVI 40000 FC 40000 FC

55-11-119 Detailed Visual Inspection of the horizontal Stabilizer Pivot Fitting

DVI 40000 FC 40000 FC

55-21-101 Detailed Visual Inspection of the Elevator Front Spar Assembly

DVI 40000 FC 40000 FC

55-21-107 Detailed Visual Inspection of the Elevator Center and Outboard Hinge Fittings

DVI 20299 FC 2744 FC

55-31-101 Detailed Visual Inspection of the Verticle Stabilizer Front Spar to Fuselage Attach Fitting

DVI 40000 FC 40000 FC




55-31-102 Detailed Visual Inspection of the Verticle Stabilizer Front Spar to Fuselage Splice Strap

DVI 40000 FC 40000 FC

55-31-104 Detailed Visual Inspection of the Verticle Stabilizer Front Spar Attachment at Vertical Stabilizer Rib 1

DVI 40000 FC 40000 FC

55-31-108 Detailed Visual Inspection of the Verticle Stabilizer Access Door Cutouts

DVI 40000 FC 40000 FC

55-31-111 Detailed Visual Inspection of the Verticle Stabilizer Pivot Fittings

DVI 40000 FC 40000 FC

55-31-112 Special Detailed Inspection of the Verticle Stabilizer Trim Actuator Pivot Structure

SDI 40000 FC 40000 FC

55-41-101 General Visual Inspection of the Verticle Stabilizer Rudder Interface

GVI 16000 FC 1600 FC EFFECTIVITY: Post-Modsum TC601R15028, No CHQ A/C effective

55-41-102 General Visual Inspection of the Verticle Stabilizer Rudder Front Spar and Skin

GVI 16000 FC 1600 FC EFFECTIVITY: Post-Modsum TC601R15028, No CHQ A/C effective

57-21-101 Special Detailed Inspection of the Drain Holes In Wing Lower Plank

SDI

6518 FC 6518 FC

EFFECTIVITY: Pre-Modsum TC601R16626 or Pre-Modsum TC601R16627. Note: The phase in compliance is as follows: 1). 53000 lb MTOW: A). For aircraft with 5518 landings or less; inspect on or before 6518 landings. B)> For aircraft with more than 5518 landings, but less than or equal to 15000 landings; inspect within the next 1000 landings. 3). For aircraft with 15000 landings or more inspect within the next 500 landings. 4). Refer to AWL 57-21-150 for alternate inspection procedure of the drain holes in lower wing plank. 5). AWL 57-21-101 or AWL 57-21-150 may be chosen. Whichever task is chosen, the task must be adhered to. An operator cannot alternate between either task.

57-21-103 Detailed Visual Inspection of the Front Spar and Lower Skin Splice at WS242.0

DVI 40000 FC 8333 FC

57-21-105 Detailed Visual Inspection of the Lower Wing Skin, between BL 0.0 to WS 314.0

DVI

30719 FC 2483 FC

PHASE−IN:Do the Threshold (initial) inspection as follows:1. For aircraft with 28719 Flight Cycles (FC) orless, accomplish before 30719 FC.2. For aircraft with 28720 FC to 30719 FC, accomplish within 2000 FC, but not later than 31719 FC. 3. For aircraft with 30720 FC or more, accomplish within1000 FC. NOTE: Subject to TC AD action

57-21-107 Detailed Visual Inspection of the Rear Spar Lower Splice Joint at BL 45.0

DVI 34188 FC 4712 FC




57-21-110 Special Detailed Inspection of the Front Spar Lower Splice Joint and Adjacent Lower Skin at WS 148.0

SDI 40000 FC 40000 FC

57-21-111 Special Detailed Inspection of the Rear Spar Lower Splice Joint and Adjacent Lower Skin at WS 148.0

SDI 40000 FC 24413 FC

57-21-112 Special Detailed Inspection of the Lower Wing Skin Splice Joints at BL 45.0, WS 65.75, and WS 148.0

SDI

21913 FC 3030 FC

EFFECTIVITY: Pre−Modsum TC601R16946. PHASE-IN: Do the threshold (initial) inspection as follows: 1). For aircraft with 18913 FC or less, inspect before 21913 FC. 2). For aircraft with 18914 FC to 21913 FC, inspect within 3000 FC, but not later than 23913 FC. 3). For aircraft with 21914 FC to 23913 FC, inspect within 2000 FC, but not later than 24913 FC. 4). For aircraft with 23914 FC or more, inspect within 1000 FC. NOTE: Subject to TC AD action

57-21-113 Detailed Visual Inspection of the Rear Spar Lower Cap at WS 168.0

DVI 40000 FC 13761 FC

57-21-114 Detailed Visual Inspection of the Front Spar Lower Cap at BL 45.0

DVI 40000 FC 7609 FC

57-21-115 Special Detailed Inspection of the Lower Skin at Rear Spar and Lower Rear Spar Web between WS 62.5 and WS 0.0

SDI24496 FC 8355 FC

NOTE: Subject to TC AD action

57-21-116 Special Detailed Inspection of the Lower Skin BL 0.0 Chordwise Splice

SDI 40000 FC 21391 FC

57-21-117 Special Detailed Inspection of the Electric Boost Pump cutoutat BL 11.0 in the Lower Aft Wing Plank

SDI

5207 FC 5207 FC

EFFECTIVITY: Pre−Modsum TC601R15850 or Pre−Modsum TC601R15999. Phase in: 1). 53000 lb MTOW: A). For aircraft with 4207 FC or less, inspect at or below 5207 FC. B). For aircraft with more than 4207 FC, but less than or equal to 9600 FC, inspect within 900 FC. 2). ALL aircraft: a). For aircraft with more than 9600 FC, inspect within 450 FC.

57-21-118 Detailed Visual Inspection of the Front Spar Lower Splice Joint at WS 29.42

DVI 40000 FC 40000 FC

57-21-119 Detailed Visual Inspection of the Wing to Fuselage Attachment at BL 45.0 and FS 513.0

DVI 40000 FC 40000 FC

57-21-120 Detailed Visual Inspection of the Wing to Fuselage Attachment and Main Landing Gear (MLG) Side Brace Fitting at BL 13.5, FS 513.0

DVI38432 FC 38432 FC




57-21-121 Special Detailed Inspection of the Wing to Inboard Flap Hinge Box Forward Attachments at WS 80.5 and WS 127.25

SDI40000 FC 40000 FC


DVI 40000 FC 40000 FC


DVI 40000 FC 40000 FC

57-21-124 Detailed Visual Inspection of the Front Spar Lower Cap and Butt Strap at WS 314.5

DVI 38008 FC 38008 FC

57-21-125 Special Detailed Inspection of the Rear Spar Lower Cap and Butt Strap at WS 314.5

SDI 40000 FC 3986 FC

57-21-127 Detailed Visual Inspection of the Wing to Outboard Flap Hinge Box Forward Attachments at WS 178.0, WS 220.0, and WS 264.0

DVI35615 FC 7275 FC

57-21-128-1 Special Detailed Inspection of the Lower Skin, Steel Strap and Main Landing Gear (MLG) Trunnion Rib at WS 65.75

SDI

35034 FC 23016 FC


57-21-128-2 Special Detailed Inspection of the Lower Skin, Steel Strap and Main Landing Gear (MLG) Trunnion Rib at WS 65.75

SDI

23356 FC 15344 FC


57-21-130-1 Detailed Visual Inspection of the Strap at WS 65.75 and Surrounding Area

DVI40000 FC 6188 FC


57-21-130-2 Detailed Visual Inspection of the Strap at WS 65.75 and Surrounding Area

DVI32047 FC 4125 FC


57-21-134 Detailed Visual Inspection of the Dry Bay Lower Access Hole Cutout at WS 314.5

DVI 40000 FC 40000 FC

57-21-135 Detailed Visual Inspection of the Lower Butt Strap and Rear Spar Lower Cap at Aileron PCU Cutouts, WS 318.3 and WS 324.4

DVI40000 FC 38043 FC

57-21-136 Detailed Visual Inspection of the Rear Spar Splice Joint at WS 353.0

DVI 40000 FC 40000 FC

57-21-138 Special Detailed Inspection of the Winglet Front Spar and Rear Spar Fittings

SDI 40000 FC 9538 FC

57-21-139 Detailed Visual Inspection of the Rib Support to Flap Hinge Box Forward Fitting at WS 80.5

DVI 40000 FC 22470 FC

57-21-140 Special Detailed Inspection of the Rib Support to Flap Hinge Box Forward Fittings at WS 127.25, WS 178.0, WS 220.0 and WS 264.0

SDI38044 FC 23714 FC

57-21-141 Special Detailed Inspection of the Lower Skin Beneath Flap Hinge Box Aft Fittings

SDI 40000 FC 11420 FC




57-21-142 Detailed Visual Inspection of the Upper Skin Access Holes Between Rear and Auxiliary Spars

DVI 40000 FC 40000 FC

57-21-143 Detailed Visual Inspection of the Aileron Hinge Fittings DVI 40000 FC 40000 FC 57-21-145-1 Special Detailed Inspection of the Main Landing Gear (MLG)

Mounting TrunnionSDI

25989 FC 9179 FC EFFECTIVITY: Pre-Modsum TC601R15827

57-21-145-2 Special Detailed Inspection of the Main Landing Gear (MLG) Mounting Trunnion

SDI17326 FC 6119 FC


57-21-146 Special Detailed Inspection of the Lower Wing Plank Access Holes at: WS 55.38 (540BB/640BB), WS 75.63 (540CB/640CB), WS 95.95 (540DB/640DB), WS 137.63 (540FB/640FB)

SDI

12271 FC 5076 FC

This task's repeat interval to be lowest interval permissable by REO 601R-57-21-030 NC A, B, C, D. Thereby insuring accomplishment of the REO within it's limits for all A/C regardless of repair status.

57-21-147 Special Detailed Inspection of the Lower Wing Plank Access Holes at: WS55.38 (540AB/640AB), WS116.83 (540EB/640EB), WS163.0 (550AB/650AB), WS185.5 (550BB/650BB)

SDI

14544 FC 6050 FC


57-21-148 Special Detailed Inspection of the Lower Wing Plank Access Holes at: WS33.75 (510BB/610BB), WS209.5 (550CB/650CB), WS231.0 (550DB/650DB), WS253.0 (550EB/650EB)

SDI

20215 FC 8301 FC


57-21-149 Special Detailed Inspection of the Lower Wing Plank Access Holes at: WS11.25 (510AB/610AB), WS274.0 (550FB/650FB), WS284.68 (550GB/650GB), WS303.86 (550HB/650HB)

SDI

40000 FC 17950 FC


57-21-150 Alternate Inspection Procedure for Drain Holes In Lower Wing Plank

SDI

6518 FC 3250 FC

EFFECTIVITY: Pre-Modsum TC601R16626 or Pre-Modsum TC601R16627 Note: AWL 57-21-101 or AWL 57-21-150 may be chosen. Whichever task is chosen, the task MUST be adhered to. An operator cannot alternate between either task. CHQ opt to perform 57-21-101.

57-21-151 Special Detailed Inspection of the Aft Lower Wing Plank at WS148.019

SDI

17621 FC 17621 FC

EFFECTIVITY: Post-Modsum TC601R15583. Note: 1). Inspection of the rear spar lower cap and splice joint at WS 148.019 are covered by AWL 57-21-111. 2). Threshold begins from the time of modification incorporation. 3). Subject to TC AD action.

57-21-152 Special Detailed Inspection of the Boost Pump Cutout in the Lower Wing Plank

SDI 6345 FC 5085 FC TR 2B-2113 EFFECTIVITY: Post-Modsum TC601R15999 Rev. B or Post SB 601R-57-032


csalsman

Rectangle



57-21-153 Special Detailed Inspection of the Aft Lower Wing Plank at WS148.019

SDI

40000 FC 40000 FC

EFFECTIVITY: Post-Modsum TC601R16015 Note: 1). Inspection of the rear spar lower cap and splice joint at WS 148.019 are covered by AWL 57-21-111. 2). Threshold begins from the time of modification incorporation.

57-21-154 Special Detailed Inspection of the Fuel Boost Pump Cutout in the Lower Wing Plank


57-21-155 Special Detailed Inspection of the Main Landing Gear (MLG) Trunnion Fitting

SDI 25989 FC 9179 FC EFFECTIVITY: Post-Modsum TC601R16268 or Post-Modsum TC601R16290

57-21-156 Special Detailed Inspection of the Lower Wing Skin Splice Joints at BL 45.0, WS 65.75 and WS 148.0, between STR 7 and STR 10 and between STR 14 and STR 17

SDI

40000 FC 2890 FC

EFFECTIVITY: Post-Modsum TC601R16626 or Post-Modsum TC601R16946

57-21-157 Special Detailed Inspection of the Drain Holes in Lower Wing Plank at BL 0.0 (STR 5 to STR 7 and STR 14 to STR 15), BL 45.0, WS 65.75 (STR 14 to STR 15) and WS 85.5

SDI

8855 FC 2610 FC


57-21-158 Special Detailed Inspection of the Drain Holes In Lower Wing Plank at BL 0.0 (STR 5 to STR 7 and STR 14), BL 45.0, WS 65.75 (STR 14 to STR 15) and WS85.5

SDI13480 FC 2850 FC


57-21-159 Special Detailed Inspection of the Boost Pump and Drain Hole Cutouts in the Lower Wing Plank

SDI 6345 FC 5085 FC TR 2B-2114 EFFECTIVITY: Post-Modsum TC601R15999 Rev. C

57-52-105 Detailed Visual Inspection of the Inboard Flap Front Spar andIntercostal Spar

DVI 40000 FC 25950 FC

57-52-106 Detailed Visual Inspection of the Inboard Flap Hinge Ribs DVI 40000 FC 40000 FC 57-52-107 Detailed Visual Inspection of the Inboard Flap Lug Plates DVI 40000 FC 36965 FC

57-52-108 Detailed Visual Inspection of the Inboard Flap Hinge Arms DVI 40000 FC 11847 FC

57-52-112 Detailed Visual Inspection of the Inboard Flap Upper and Lower Skin

DVI 40000 FC 14900 FC

57-52-113 Detailed Visual Inspection of the Inboard Flap Hinge Arms DVI 40000 FC 11070 FC

57-52-114 Detailed Visual Inspection of the Inboard Flap Vane Actuator Tube Assembly

DVI 26239 FC 26239 FC

57-52-118 Special Detailed Inspection of the Inboard Flap Vane Skin SDI 40000 FC 40000 FC

57-52-119 Special Detailed Inspection of the Inboard Flap Vane Mounting Structure

SDI 40000 FC 40000 FC

57-53-102 Detailed Visual Inspection of the Outboard Flap Upper and Lower Skin

DVI 40000 FC 40000 FC

57-53-103 Special Detailed Inspection of the Outboard Flap Front Spar SDI 40000 FC 40000 FC


csalsman

Rectangle

csalsman

Small Stamp



57-53-104 Detailed Visual Inspection of the Outboard Flap Vane Support Structure

DVI 40000 FC 32690 FC

57-53-105 Detailed Visual Inspection of the Outboard Flap Vane Mounting Lug/Nose Riblet

DVI 40000 FC 40000 FC

57-53-106 Detailed Visual Inspection of the Outboard Flap Hinge Support Structure

DVI 40000 FC 22253 FC

57-53-107 Detailed Visual Inspection of the Outboard Flap Nose Riblets at Flap Arm Locations

DVI 40000 FC 40000 FC

57-53-110 Special Detailed Inspection of the Outboard Flap Intercostal Spar Machining

SDI 40000 FC 10487 FC

57-53-114 Detailed Visual Inspection of the Outboard Flap Hinge Arms DVI 40000 FC 3893 FC

57-53-118 Special Detailed Inspection of the Outboard Flap Hinge Box to Flap Attachment Structure

SDI 40000 FC 35167 FC

57-53-122 Detailed Visual Inspection of the Outboard Flap Vane DVI 40000 FC 40000 FC 57-53-125 Composite outboard flap components DVI 40000 FC 40000 FC EFFECTIVITY: Post-Modsum TC601R2550057-54-103 Special Detailed Inspection of the Inboard Flap Hinge Boxes

Including End FittingsSDI 16500 FC 4600 FC

57-54-105 Special Detailed Inspection of the Outboard Flap Hinge Boxes Including End Fittings

SDI 16000 FC 16000 FC

57-61-101 Detailed Visual Inspection of the Aileron Center Fitting DVI 40000 FC 40000 FC 57-61-102 Detailed Visual Inspection of the Aileron Lower Skin Panel DVI 40000 FC 40000 FC

57-61-104 Detailed Visual Inspection of the Aileron Front Spar DVI 40000 FC 40000 FC 57-61-105 Detailed Visual Inspection of the Aileron Internal Structure DVI 40000 FC 40000 FC

57-61-106 Detailed Visual Inspection of the Aileron Hinge Fittings and Back-Up Structure

DVI 16000 FC 1600 FC EFFECTIVITY: Post-Modsum TC60R15307, No CHQ A/C effective.

57-61-107 Detailed Visual Inspection of the Aileron Upper and Lower Skin

DVI 16000 FC 1600 FC EFFECTIVITY: Post-Modsum TC60R15307, No CHQ A/C effective.

57-61-108 Special Detailed Inspection of the Aileron Front Spar and Front Spar Splice

SDI 16000 FC 1600 FC EFFECTIVITY: Post-Modsum TC60R15307, No CHQ A/C effective.

57-61-109 Special Detailed Inspection of the Aileron Side Hinge Pins SDI 16000 FC 1600 FC EFFECTIVITY: Post-Modsum TC60R15307, No CHQ A/C effective.

71-21-101 Special Detailed Inspection of the Engine Mount Yoke Fitting SDI 40000 FC 15670 FC

71-21-102 Special Detailed Inspection of the Engine Mount Thrust Fitting

SDI 40000 FC 16776 FC

71-21-103 Special Detailed Inspection of the Engine Mount Upper Link of Yoke Fitting at FS 625.3

SDI 40000 FC 20460 FC

71-21-104 Special Detailed Inspection of the Engine Mount Shaft SDI 26316 FC 11831 FC




C21-50-115-01 Decompression Equalizer Rubber Diaphragm. Visual Inspection that Diaphragm is Positioned Correctly and thus Sealing Off Compartment

VC10000 FH 10000 FH

CMR ** Note: May Require Removal of Tunnel Fairing or Use of Borescope

C24-10-129-01 Functional Check of the GCU No. 1, No. 2 and No. 3 for Overvoltage

FC 4000 FH 4000 FH CMR *

C24-20-129-01 Functional Check of the Air Driven Generator (ADG) FC 4000 FH 4000 FH CMR *C25-17-152-01 Functional Check of the fortified flight compartment door

pressure relief latch.FC 5000 FH 5000 FH CMR ** EFFECTIVITY: Post-Modsum TC601R101329

C26-10-131-01 Operational Check of the APU Fire Diode CRIWG Check for Open Circuit

OP 10000 FH 10000 FH CMR **

C26-20-131-01 Visual Check of the APU Firex Tubing for Damage and Security

VC 10000 FH 10000 FH CMR **

C26-20-131-02 Operational Check of the Engine, Jetpipe, and APU Fire Detection Systems Test

OP 100 FH 100 FH CMR **

C26-20-131-03 Operational Check of the APU Fire Extinguishing System OP 100 FH 100 FH CMR **C27-10-105-01 Operational Check of the Disconnect Facility OP

1000 FH 1000 FH

CMR * Disconnect and check the SPOILERON ROLL message on EICAS. Press PILOT PRIORITY SW and verify message extinguish and PBA revert to green. Also verify a new green PILOT ROLL CMD message on EICAS. Verify full free travel of pilots channel and surfaces response. Press COPILOT PRIORITY SW and verify priority transfer and full free travel of copilot's channel and surfaces response.

C27-10-105-03 Operational Check of the Tension Regulator, Bungee Breakout Mechanism, the Priority Switch and Auto Priority Latch Relay

OP10000 FH 10000 FH

CMR **

C27-10-105-05a Functional Check of Each Rudder PCU for Backlash and Deflection Under Load

FC 5000 FH 5000 FH CMR *

C27-10-105-05b Functional Check of Each Elevator PCU for Backlash and Deflection Under Load

FC 5000 FH 5000 FH CMR *

C27-10-105-06 Functional Check of Each Aileron PCU for Internal Leakage. FC 5000 FH 5000 FH CMR *

C27-10-105-07 Check the Flutter Dampers Fluid Level, the Operation of the Low Level Switch, the Shear Rivets Integrity and the Security of Attachment

VC5000 FH 5000 FH

CMR **

C27-20-108-01 Verify Freedom of Movement of Each PCU Input TelescopingJam Tolerant Bungee

OP 10000 FH 10000 FH CMR *

C27-30-102-01 Operational Check of the Mechanical Disconnect System OP 10000 FH 10000 FH CMR **C27-30-102-03 Verify Freedom of Movement of Each PCU Input Telescoping

Jam Tolerant Mechanism BungeeOP 5000 FH 5000 FH CMR *

C27-30-102-05 Check the Flutter Dampers Fluid Level, the Operation of the Low Level Switch, the Shear Rivets Integrity and the Security of Attachment

VC10000 FH 10000 FH

CMR *


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C27-31-102-01 Functional Check of the Pitch Feel Simulator (PFS ) to Detect Loss of Feel force On the Control Column from PFS Internal Disconnect, Input Lever Disconnect, and Detached Pushrod

FC

10000 FH 10000 FH

CMR *

C27-35-112-01 Operational Check of the FCP Disengage Circuit and AP/SP Disc Switches

OP 5000 FH 5000 FH CMR **

C27-35-112-02 Operational Check of the Flap Position Inputs from the Flap Position Transmitter Unit to the Stall Protection Computer (MDC BITE)

OP500 FH 500 FH

CMR * Post Modsum TC601R15984, No CHQ A/C effective

C27-40-103-01 Task Deleted TR 2A-32C27-40-113-01 Operational Check of the Horizontal Stabilizer Trim System OP 100 FH 100 FH CMR **

C27-42-103-01 Detailed Inspection of the HSTA Secondary Load Path Indicator

DI

5000 FH 5000 FH

CMR * Note: For Aircraft with 4500 HSTA flight hours or less, inspect at or before 5000 HSTA flight hours, and every 5000 flight hours thereafter......For Aircraft with more than 4500 HSTA flight hours, inspect within the next 500 HSTA flight hours, and every 5000 flight hours thereafter.....Airworthiness Directive Issued.

C27-50-111-01 Functional Check (Backlash) of Flap Actuator FC

1000 FH 1000 FH

CMR TR 2A-37 * EFFECTIVITY: IB Flap Actuators: P/N 601R93101-9 (P/N 852D100-11) or lower. OB Flap Actuators: P/N 601R93103-18 (P/N 853D100-18) or lower, P/N 601R93104-10 (P/N 854D100-12) or lower. Phase-In: Do the initial functional check within 500 Flight Hours from the issue date of this TR.

C27-50-111-03 Detailed Inspection of the Flap Actuator Lug and Trunnion Housing

DI

500 FH 500 FH

CMR TR 2A-37 ** EFFECTIVITY: IB Flap Actuators: P/N 601R93101-9 (P/N 852D100-11) or lower. OB Flap Actuators: P/N 601R93103-18 (P/N 853D100-18) or lower, P/N 601R93104-10 (P/N 854D100-12) or lower. Phase-In: Do the initial functional check within 500 Flight Hours from the issue date of this TR.

C27-50-111-05 Functional Check (BITE) of the Flap Electronic Control Unit (FECU)

FC 5000 FH 5000 FH CMR *

C27-50-111-06 Discard of the flap actuator DS

4000 FH 4000 FH

CMR TR 2A-38 * EFFECTIVITY: IB Flap Actuators: P/N 601R93101-9 (P/N 852D100-11) or lower. OB Flap Actuators: P/N 601R93103-18 (P/N 853D100-18) or lower, P/N 601R93104-10 (P/N 854D100-12) or lower. No CHQ A/C effective. Phase-In: Do the discard within 4000 Flight Hours from the issue date of this TR or before March 31, 2008, whichever comes first.


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C27-50-111-07 Detailed Inspection of the Flap Actuator for Structural Integrity and External Disconnect

DI

1000 FH 1000 FH

CMR TR 2A-38 * EFFECTIVITY: IB Flap Actuators: P/N 601R93101-19 (P/N 852D100-19) and subs. OB Blap Actuators: P/N 601R93103-19, -20 (P/N 853D100-19, -20) and subs, P/N 601R93104-19, -20 (P/N 854D100-19, -20) and subs.

C27-50-111-08 Operational Check (IBIT) of the Skew Detection Unit (SDU) for Dormant Failures

OP 500 FH 500 FH CMR * EFFECTIVITY: Post-Modsum TC601R15480 or Post SB 601R-27-116

C27-50-111-09 Functional Check of the Flap Actuator for Internal Disconnect FC

1000 FH 1000 FH

CMR TR 2A-39 * EFFECTIVITY: IB Flap Actuators: P/N 601R93101-19 (P/N 852D100-19) and subs. OB Blap Actuators: P/N 601R93103-19, -20 (P/N 853D100-19, -20) and subs, P/N 601R93104-19, -20 (P/N 854D100-19, -20) and subs.

C27-50-111-10 Functional Check of the Outboard Flap Actuator Torque Limiter

FC

14000 FC 14000 FC

CMR TR 2A-39 * EFFECTIVITY: OB Flap Actuators: P/N 601R93103-19. -20 (P/N 853D100-19, -20) and subs,P/N 601R93104-19, -20 (P/N 854D100-19, -20) and subs.

C27-50-111-11 Functional Check of the Inboard Flap Actuator Torque Limiter(See Note)

FC

10666 FC 10666 FC

CMR TR 2A-39 * EFFECTIVITY: IB Flap Actuators: P/N 601R93101-19 (P/N 852D100-19) and subs. Note: Replace the following components: Pinion Seals, Retaining Ring (Snap Ring), and Needle Bearings.

C27-50-111-12 General Visual Inspection of the visual portion of the attachment on the inboard flap actuatorsfor condition and security

GVI

100 FH 100 FH

CMR EFFECTIVITY:IB Flap Actuators: P/N 601R93101−9 (P/N 852D100−11) or lowerPHASE−IN:Do the initial inspection within 100 Flight Hours from the issue date of TR 2A−40 (Feb 23/07).

C27-50-300-01 Functional Check of the Inboard Flap Actuator for Flap LinearActuator Endplay

FNC2000 FH 2000 FH

CMR EFFECTIVITY: IB Flap Actuators: P/N: 601R93101-19 (P/N: 852D100-19)

C27-60-106-01 Disconnect and check the SPOILERON ROLL message on EICAS.

OP

1000 FH 1000 FH

CMR ** Press PILOT PRIORITY SW and verify message extinguish and PBA revert to green. Also verify a newgreen PILOT ROLL CMD message on EICAS. Verify that ARINC Label 351 BIT 11 is NOT SET. Verify full free travel of pilots channel and surfaces response. Press COPILOT PRIORITY SW and verify priority transfer and full free travel of copilot's channel and surfaces response. Verify that ARINC Label 351 BIT 12 is NOT SET.




C28-00-142-01 Operational Check of the Fuel Crossflow OP

100 FH 100 FH

CMR ** Verify X-FLOW AUTO OVERRIDE switch light pressed out. Verify no MAN XFLOW message. Push in GRAVITY X-FLOW switch light and verify: - OPEN light/GRAVITY X-FLOW message. Push out GRAVITY X-FLOW and verify: -light/message off.

C28-20-131-01 Functional Check of the APU Fuel Fire Shut Off Valve FC5000 FH 5000 FH

CMR * Disconnect Plumbing Downstream and Verify No Leakage with Valve Closed and Pump Running (suchas when fuel filter is removed).

C30-10-141-01 Functional Check of the Overheat Sensors and Standby Overheat Switches

FC

4000 FH 4000 FH

CMR * Perform the functional check by applying heat at each switch/sensor location. Verify WING OVHT message at specific temperature for each switch. NOTE: In order to check the standby sensor the system power must be off.

C30-10-141-02 Operational Checkof the Anti-Ice Duct System Self-Test OP 100 FH 100 FH CMR **C31-40-158-01 Operational Check of the Data Concentrator Unit (DCU)

Output Busses of the Engine Data to the Displays and DCUs Bus Transmitter Circuitry

OP5000 FH 5000 FH

CMR ** Operational check of each individual DCU transmission during engine run by de-activating the other DCU. NOTE: 2 DCU configuration only!

C34-10-141-01 Functional Check of the Altimeter Scale Error FC

24 MO 24 MO

CMR * TR 2A−19 EFFECTIVITY: Post SB601R−34−080 or CR34−365 With ADC−850A P/N 822−0372−143/−445 and Post VSB Rockwell Collins ADC−850 () −34−63 or, All other ADC−850A Part Numbers. NOTE: The time interval refers to ADC component time and is counted from the date of the last ADC test.

C34-10-141-03 Functional Check of the Altimeter Scale Error FC

8 MO 8 MO

CMR * TR 2A-19 EFFECTIVITY: Post SB601R-34-080 or CR34-365 With ADC-850A P/N 822-0372-143/-445 and Pre VSB Rockwell Collins ADC-850 () -34-63. NOTE: The time interval refers to ADC component time and is counted from the date of the last ADC test.

C34-40-107-01 Windshear Warning System Check FC

10000 FH 10000 FH

CMR ** EFFECTIVITY:Pre−Modsum TC601R15059ORPre−SB 601R−31−022

C35-10-128-01 Verify Correlation Between the Crew Oxygen Pressure Indication on EICAS, the Refill Panel, and that on the Direct Reading Gage Attached to the Bottle

OP500 FH 500 FH

CMR *

C36-20-133-01 Operational Check of the Bleed Air Leak Detection System Test-Loop A

OP

500 FH 500 FH

CMR ** On the BLEED AIR Panel select DUCT MON switch to LOOP A and verify: -DUCT MON LOOP A MESSAGE on secondary EICAS. Select switch to BOTH.




C36-20-133-02 Operational Check of the Bleed Air Leak Detection System Test-Loop B

OP

500 FH 500 FH

CMR ** On the BLEED AIR Panel select DUCT MON switch to LOOP B and verify: -DUCT MON LOOP B MESSAGE on secondary EICAS. Select switch to BOTH.

C52-10-821-01 Ensure that Upper Latch Pins Are Correctly Installed and Functional

FC 4000 FH 4000 FH Post-Modsum TC601R13193

F12-20-00-01 Clean Windshield to Remove Foreign Object Contamination Clean Wing Leading Edges to Remove Foreign Objects and Contamination, and Insure Sealant Does Not Protrude Above the Skin Surface

SV

3 DY 3 DY

R22-11-A083-01 Lubrication of the Aileron Autopilot Servo and Servo Mount Engage Clutch Faces

LU6500 FH 6500 FH

PHASE IN: For aircraft with more than 5400 FH, do this task no later than 1100 FH from Nov 5/04. NOTE: Airworthiness Directive Issued.

R27-00-A053-01 Discard of the Aileron Control Pulleys DS

10500 FH 10500 FH

LIFE EFFECTIVITY: P/N 600-90800-2 (Outboard wing zone 591/691 qty 4) and P/N 600-90800-5 (Aileron zone 599/699 qty 4) PHASE IN: For aircraft with more than 9500 FH, do this task no later than 1000 FH from Nov 5/04. NOTE: Airworthiness Directive Issued.

R27-11-A082-01 Lubrication of the Aileron Control Cables at the Wing Pulley Interfaces

LU5500 FH 5500 FH


R27-11-A082-02 Lubrication of the Aileron Rear Quadrant and Trim Lever Bearings

LU5500 FH 5500 FH


R27-31-A024-01 Task Deleted per Rev. 7 Part 2 MRM.R27-50-300-01 Restoration of the Outboard Flaps Actuator (see Note) RS

20000 FC 20000 FC

EFFECTIVITY: Canadair P/N 601R93103−19/ −20 and 601R96104−19/ −20 (Vendor P/N 853D100−19/ −20 and 854D100−19/ −20) Note: Discard the following components at restoration: 1) Seal P/N 853SC177−1, 2) Retaining Ring P/N SA13408−1, 3) Outboard Thrust Bearing P/N SC14000−062, 4) Outboard Thrust Race P/N SC14002−062A, and 5) Backup Ring P/N 853B143−1.




R32-31-828-01 Detailed Visual Inspection of the Landing Gear Control Handle Slider

DVI

1000 FC 1000 FC

Note: This inspection requirement applies to Landing Gear Control Handle Assemblies Canadair P/N 601R50967−7 (Vendor P/N 7−45502−1) with suffix "B" after the serial number and Canadair P/N 601R50967−9 (Vendor P/N 7−45502−3) ONLY. No CHQ A/C effective. For Landing Gear Control Handle Assemblies that have been in service for more than 850 flight cycles on Jan 9/01, Inspection is required with in the next 150 flight cycles.

R32-31-828-02 Restoration of the Landing Gear Control Handle Assembly RS

300 FC 300 FC

Canadair P/N 601R50967−7 (Vendor P/N 7−45502−1) with Suffix "A" After Serial Number. Note: For Landing Gear Control Handle Assemblies that have been in service for more than 150 flight cycles on Jan 9/01, restoration is required within the next 150 flight cycles (refer to Alert Service Bulletin A601R−32−083).

R32-31-828-03 Restoration of the Landing Gear Control Handle Assembly RS

4000 FC 4000 FC

Canadair P/N 601R50967-7 (Vendor P/N 7-45502-1) with Suffix "B" after Serial Number and Canadair P/N 601R50967-9 (Vendor P/N 7-45502-3)

R52-11-878-01 Detailed Inspection of the Phase IV Passenger Door Upper Latch Fitting Sleeve Bushings for Migration

DI600 FH 600 FH

Post-Modsum TC601R13193 and Pre-Modsum TC601R15596 or Pre SB 601R-52-110, A/C 459, 461.

R72-21-802-01 Visual Check of the Engine Master Chip Detector Indicator VC30 FH / 3 DY 30 FH / 3 DY

Pre GE SB 72-0109

REO 601R-32-10-008 NC Discard of the Main Landing Gear (MLG) Trailing Arm DS TBD TBD LIFE P/N 17084-5 and S/N DCL-076REO 601R-32-11-047 NC Discard of the Main Landing Gear (MLG) Main Fitting

AssemblyDS TBD TBD LIFE P/N 17064-104 and S/N DCL-174

REO 601R-32-11-161 NC Discard of the Main Landing Gear (MLG) Pivot Pin DS TBD TBD LIFE P/N 17041-1 and S/N DCL-175REO 601R-32-11-171 NC Discard of the Main Landing Gear (MLG) Pivot Pin DS TBD TBD LIFE P/N 17041-1 and S/N DCL-218REO 601R-32-11-182 NC Discard of the Main Landing Gear (MLG) Pintle Pin DS TBD TBD LIFE P/N 17040-1 S/N DCL 030REO 601R-32-11-183 NC Discard of the Main Landing Gear (MLG) Pintle Pin DS TBD TBD LIFE P/N 17040-1 S/N DCL-026REO 601R-32-21-109 NC Discard of the Nose Landing Gear (NLG) Piston (Piston

Tube)DS TBD TBD LIFE P/N 16120-1 and S/N B20-10

REO 601R-53-00-026 A Generic Repair to Cabin Window Surround Structure SDI 10047 FC 10047 FC REO 601R-53-00-030 C-a Generic Repair to Fuselage Skin Around Passenger Door

Upper Corner and Lower CornersDVI 20283 FC 16750 FC

REO 601R-53-00-030 C-b Generic Repair to Fuselage Skin Around Passenger Door Upper Corners

SDI 40000 FC 40000 FC

REO 601R-53-00-033 C-a Generic Repair to Fuselage Skin Around Service Door Cut-Out Lower Corners

SDI 40000 FC 40000 FC




REO 601R-53-00-033 C-b1 Generic Repair to Fuselage Skin Around Service Door Cut-Out Edges of the Door

SDI 40000 FC 40000 FC Note 4

REO 601R-53-00-033 C-b2 Generic Repair to Fuselage Skin Around Service Door Cut-Out Edges of the Door

DVI 40000 FC 18858 FC Note 4

REO 601R-53-00-034 D Generic Repair to Fuselage Skin Assembly, Non-Flush Baggage Compartment

SDI40000 FC 14579 FC

Note: These Repair inspection intervals Supersede AWL 53-61-141 inspection requirements for the repaired corner.

REO 601R-53-00-061 A Deleted, transferred to GREO per Rev. 7 Part 2 MRM. REO 601R-53-11-006 NC, A, B, C Repair to Fuselage Skin, FS 235.00 SDI 15000 FC 11400 FC REO 601R-53-11-010 NC, A, B, C Repair to Fuselage Skin, FS 235.00 SDI 15000 FC 11400 FC REO 601R-53-11-048 A Repair to Fuselage Skin Radius, FS 235.00 SDI

35220 FC 25159 FC

EFFECTIVITY: 7003 and Up. Note: This inspection Supersedes the inspection method and interval for AWL 53-11-124, for aircraft incorporating this REO.

REO 601R-53-11-162 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM. REO 601R-53-11-276 NC-1 Repair to Bulkhead Channel FS 202.75, LBL30.00, WL65.00 SDI 14874 FC 7693 FC EFFECTIVITY: 7003 to 7196 Note 4

REO 601R-53-11-276 NC-2 Repair to Bulkhead Channel FS 202.75, LBL30.00, WL65.00 DVI 14874 FC 5483 FC EFFECTIVITY: 7003 to 7196 Note 4

REO 601R-53-21-180 NC-1 Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-21-180 NC-2 Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-21-183 NC-1 Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-21-183 NC-2 Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-21-313 NC-1 Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-21-313 NC-2 Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-31-012 C or D-1 Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-31-012 C or D-2 Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-31-019 NC to C Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-41-010 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-41-057 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-41-067 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-41-102 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-41-103 A Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-53-61-1240 NC-1 Repair and Modification to FS 621.00 Pressure Bulkhead

WebSDI 40000 FC 23860 FC TR 2B-2117 Note 4

REO 601R-53-61-1240 NC-2 Repair and Modification to FS 621.00 Pressure Bulkhead Web

DVI 40000 FC 8455 FC TR 2B-2117 Note 4

REO 601R-53-61-1285 NC-1 Repair to FS 621.00 Pressure Bulkhead Web SDI 40000 FC 23860 FC TR 2B-2117 Note 4REO 601R-53-61-1285 NC-2 Repair to FS 621.00 Pressure Bulkhead Web DVI 40000 FC 8455 FC TR 2B-2117 Note 4REO 601R-53-61-345 D-a Generic Repair to Engine Support Beam Upper and Lower

Webs Upper Doubler, LBL 18.0 to RBL 18.0, and Lower Doubler, LBL 9.5 to RBL 9.5

SDI8350 FC 8350 FC

EFFECTIVITY: Pre-Modsum TC601R15054 or Pre SB 601R-53-059 Rev. A or later.




REO 601R-53-61-345 D-b Generic Repair to Engine Support Beam Upper and Lower Webs Upper Doubler, Outboard of LBL 18.0 and RBL 18.0, and Lower Doubler, Outboard of LBL 9.5 and RBL 9.5

DVI

8350 FC 1485 FC

EFFECTIVITY: Pre-Modsum TC601R15054 or Pre SB 601R-53-059 Rev. A or later.

REO 601R-53-61-358 A Repair to Engine Support Beam Lower Web SDI 5885 FC 5885 FC EFFECTIVITY: Pre-Modsum TC601R15054 or Pre SB 601R-53-059 Rev. A or later.

REO 601R-53-61-366 E-a Repair to Engine Support Beam Lower Web - Web and Doubler Outboard of BL 36.25

SDI 20288 FC 14896 FC Note: Threshold interval begins from the time of repair incorporation

REO 601R-53-61-366 E-b Repair to Engine Support Beam Lower Web - Web, Splice and Cap Angle

SDI 12509 FC 12509 FC Note: Threshold interval begins from the time of repair incorporation

REO 601R-53-61-368 NC Deviation to REO 601R-53-61-345 SDI 8350 FC 8350 FC REO 601R-53-61-530 NC Deviation to REO 601R-53-61-345, Upper Web SDI 8350 FC 8350 FC REO 601R-53-61-531 NC Deviation to REO 601R-53-61-345, Lower Web SDI 8350 FC 8350 FC REO 601R-53-61-870 B Repair to Engine Support Beam Upper and Lower Webs SDI TBD TBD REO 601R-55-11-061 NC-a Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-55-11-061 NC-b Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-55-21-080 NC-a Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-55-21-080 NC-b Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-55-21-082 NC-a Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-55-21-082 NC-b Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-57-21-030 NC A, B, C, D

Repair to Wing Lower Plank Access Holes SDI

See Note See Note

This REO will be accomplished by lowering the Repeat Limit on the following AWL's to the lowest interval permitted per this REO regardless of repair status: 57-21-146, 57-21-147, 57-21-148, 57-21-149.

REO 601R-57-21-037 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-57-21-046 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-57-21-130 C Repair to Lower Wing Plank WS 148.019, LH and RH SDI

35550 FC 17566 FC Note: Threshold begins from the time of aircraft entry-

into-service and NOT from the time of repair incorporation.

REO 601R-57-21-131 NC Deviation to REO 601R-57-21-130 SDI35550 FC 17566 FC

Note: Threshold begins from the time of aircraft entry-into-service and NOT from the time of repair incorporation.

REO 601R-57-21-169 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-57-61-004 B Deleted, transferred to GREO per Rev. 7 Part 2 MRM.REO 601R-57-61-052 NC Deleted, transferred to GREO per Rev. 7 Part 2 MRM.


Chapter 6FSL Maintenance Program


FSL Maintenance Program

IntroductionThe section following contains the various maintenance and inspection tasks that encompass the Fuel System Limitation tasks. These tasks are defined as DetailedVisual Inspections (DI/DVI) and Functional Checks (FC/FNC). They are performed to the ensure the inherent safety and reliability levels of the equipment. They alsoensure that the safety and reliability of items are restored to their inherent levels when deterioration has occurred.









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Maintenance Time Limitations Manual CRJ200 Chapter 6: FSL


28-11-00-601 Detailed Inspection of the Critical Bonding Jumpers for Corrosionand Damage

DI

20000 FH 20000 FH AD

EFFECTIVITY:Post−Modsum TC601R16091ORPost−SB 601R−28−055PHASE−IN:For aircraft with more than 15000 Flight Hours, inspect within the next 5000 Flight Hours. AD 2008-06-02 effective date supercedes this task

28-11-00-602 Functional Check of the Critical Bonding Jumpers FC

20000 FH 20000 FH AD

EFFECTIVITY:Post−Modsum TC601R16091ORPost−SB 601R−28−055PHASE−IN:For aircraft with more than 15000 Flight Hours, inspect within the next 5000 Flight Hours. AD 2008-06-02 effective date supercedes this task

28-11-00-603 Detailed Inspection of the Sealant on the In - Tank LRUs DI20000 FH 20000 FH AD

Phase In: For Aircraft with More than 15000 Flight Hours, Inspect within the Next 5000 Flight Hours. AD 2008-06-02 effective date supercedes this task

28-11-00-604 Detailed Inspection of the fuel tank wiring harness clipping along the front and rear spar of the center andwing fuel tanks for condition and security

DI

20000 FH 20000 FH AD

TR 2D-4 EFFECTIVITY:Post−Modsum TC601R16139 AND Post−Modsum TC601R25270ORPost−SB 601R−28−059PHASE−IN:For aircraft with more than 15000 Flight Hours, inspect within the next 5000 Flight Hours. AD 2008-06-02 effective date supercedes this task

29-33-01-601 Functional Check of the Hydraulic System No. 1, No. 2, and No. 3 Reservoir Temperature Transducer

FC5000 FH 5000 FH AD

TR 2D-3 Phase In: For ALL aircraft, inspect within the next 5000 Flight Hours. AD 2008-06-02 effective date supercedes this task

29-33-01-602 Discard of the Hydraulic System No. 1, No. 2, and No. 3 Reservoir Temperature Transducer

DS30000 FH 30000 FH AD

LIFE

TR 2D-3 Phase In: For ALL aircraft, with more than 25000 Flight Hours, inspect within the next 5000 Flight Hours

Revision 1 / April 15, 2008 Chapter 6: FSL 1 of 1

Chapter 7CPCP Program


CPCP Program

IntroductionThe section following contains the various inspection tasks that encompass the Corrosion Prevention and Control Program (CPCP) Inspection tasks. These tasks aredefined as General Visual Inspections (GVI), Detailed Visual Inspections (DI/DVI), and Special Detailed Inspections (SDI). They are performed to ensure the inherentsafety and reliability levels of the equipment. They also ensure that the safety and reliability of items are restored to their inherent levels when deterioration has occurred.

Corrosion LevelsCorrosion levels have been established to relate the extension of degradation due to corrosion that

affects primary structure during repeat scheduled inspections. The following three levels of corrosion

definitions are applicable to this program:

• Level 1 Corrosion

Corrosion occuring between successive inspections that can be reworked/blended-out, within

allowable limits as defined by Bombardier Aerospeace Regional Aircraft and does not require

structural reinforcement or replacement.

OR

Corrosion damage that exceeds allowable limits and could require structural reinforcement, but can

be attrributed to an event not typical of the operator’s usage of other aircraft in the same fleet (e.g.

mercury spill, chemical spill); and is not of critical airworthiness concern.

OR

Operator experience has demonstrated only light corrosion between successive inspections but latest

inspection and cumulative blend-out now exceeds the allowable limits and could require structural

reinforcement or replacement.

Chapter 7CPCP Program



Corrosion occuring between successive inspections that requires a single rework/blend-out, which

exceeds allowable limits and requires a repair/reinforcement or complete or partial replacement of a

structural significant item or principal structural element, but is not a critical airworthiness concern.

NOTECorrosion findings which are discovered at the Threshold and that require repair or replacement of structure, should be treated as Level 2or 3 findings for reporting and program evaluation.


Corrosion found during first or successive inspections, which is determined to be an urgent

airworthiness concern requiring immediate action.

NOTE 1 Level 3 corrosion will normally be determined by the operator, however, Bombardier Aerospace Regional Aircraft can be contacted to participatewith this determination.

NOTE 2 When Level 3 corrosion is found, consideration should be given to action required on other aircraft in the operator’s fleet. Details of the corrosion findingsand planned action(s) should be immediately reported to the appropriate regulatory authority.





• Threshold - Indicates the maximum specified interval for the scheduled task of that item. Intervals are specified in calendar months unless indicatedotherwise

• Repeat - Identifies the repeat interval for the scheduled task. Intervals are specified in calendar months unless indicated otherwise



Maintenance Time Limitations Manual CRJ200 Chapter 7: CPCP


52-11-03-01 Detailed Inspection of the Passenger Door Internal Structure DI 72 MO 72 MO 52-21-03-01 Detailed Inspection of the Overwing Emergency Exit Internal Structure DI 48 MO 48 MO 52-31-03-01 Detailed Inspection of the Cargo Door Internal Structure DI 96 MO 48 MO 52-41-03-01 Detailed Inspection of the Service Door Internal Structure DI 48 MO 48 MO 53-11-02-01 Detailed Inspection of the FS 202.75 Forward Pressure Bulkhead Aft Face DI 72 MO 72 MO 53-11-03-01 Detailed Inspection of the FS 210.0, FS 220.0, FS 235.0, FS 250.0, and FS 265.0

Frames Below WL 110.0 (Window Structure)DI 96 MO 72 MO

53-11-08-01 Detailed Inspection of the Internal Skin and Stringers Below WL 110.0 (Window Structure)

DI 96 MO 72 MO

53-11-10-01 Detailed Inspection of the Flight Compartment Floor Beams and Crossmembers DI 96 MO 72 MO

53-21-01-01 Detailed Inspection of the Passenger Door Upper and Lower Sills DI 96 MO 72 MO 53-21-02-01 Detailed Inspection of the Passenger Door Interior Cutout Frames at FS 310.0 and

FS 349.0, and Interior Backup StructureDI 96 MO 72 MO

53-21-08-01 Detailed Inspection of the Service Door Interior Side Frames, Upper and Lower Sills, and Backup Structure

DI 96 MO 72 MO

53-21-10-01 Detailed Inspection of the Avionics Compartment Door Cutout Surrounding Structure

DI 48 MO 48 MO

53-21-11-01 Detailed Inspection of the Floor Support Structure from FS 280.0 to FS 409.0 DI 48 MO 48 MO 53-21-14-01 Detailed Inspection of the Internal Skin Panels, Frames and Stringers Below Floor

from FS 280.0 to FS 409.0DI 96 MO 72 MO

53-41-01-01 Detailed Inspection of the Floor Support Structure, FS 409.0 to FS 409.0 + 128 (Including Floor Beams, Struts, Floor Sills, and Seat Rails)

DI 48 MO 48 MO

53-41-04-01 Detailed Inspection of the Interior Skin Panels, Frames and Stringers Below Floor, FS 409.0 to FS 409.0 + 128

DI 96 MO 72 MO

53-41-08-01 Detailed Inspection of the forward Keel Beams, FS 409.0 + 80 to FS 409.0 + 112 DI 96 MO 72 MO

53-41-09-01 Detailed Inspection of the Forward Keel Beam Pressure Box, FS 409.0 + 112 to FS 409.0 + 128

DI 96 MO 72 MO

53-41-16-01 Detailed Inspection of the Aft Face of Frame FS 409.0 + 128 Below Floor DI 72 MO 72 MO 53-41-18-01 Detailed Inspection of the Aft Face of Fuselage Frame FS 559.0 Below Floor DI 72 MO 72 MO 53-41-20-01 Detailed Inspection of the Overwing Emergency Exit Cutout Surround Structure DI 96 MO 72 MO

53-41-24-01 Detailed Inspection of the Upper Surface of Pressure Floor Sill Structure, FS 409.0 + 128 to FS 559.0, BL36 to BL47, LHS and RHS

DI 96 MO 72 MO

53-41-26-01 Detailed Inspection of the Frame FS 424.0 Wing Attachment Lugs DI 96 MO 72 MO 53-41-29-01 Detailed Inspection of the Frame FS 473.15 Wing Attachment Lugs DI 96 MO 72 MO 53-41-32-01 Detailed Inspection of the Frame FS 513.0 Wing Attachment Links DI 48 MO 48 MO 53-41-33-01 Detailed Inspection of the Overwing Floor Support Beam at FS 460.0 DI 96 MO 72 MO 53-41-34-01 Detailed Inspection of the Pressure Floor Skin Panel Upper Surface FS 409.0 + 128

to FS 559.0, BL 36L to BL 36RDI 96 MO 72 MO

53-41-35-01 Detailed Inspection of the Pressure Floor Skin Panel Lower Surface FS 409.0 + 128 to FS 559.0, BL 36L to BL 36R

DI 96 MO 72 MO

53-41-36-01 Detailed Inspection of the Pressure Floor Support Beams, FS 409.0 + 128 to FS 559.0

DI 48 MO 48 MO

Revision 1 / April 15, 2008 Chapter 7: CPCP 1 of 2

Maintenance Time Limitations Manual CRJ200 Chapter 7: CPCP


53-41-38-01 Detailed Inspection of the Lower Surface of Pressure Floor Sill Plate and Intercostals, FS 409.0 + 128 to FS 513.0, BL36 BL47, LHS and RHS

DI 96 MO 72 MO

53-41-39-01 Detailed Inspection of the Frame to Longeron "T" Brackets at Pressure Floor Sill DI 96 MO 72 MO

53-41-40-01 Detailed Inspection of the Underfloor Longeron Assembly, LHS and RHS DI 96 MO 72 MO 53-41-42-01 Detailed Inspection of the Forward Keel Beam Lugs and Links DI 72 MO 72 MO 53-41-44-01 Detailed Inspection of the Floor Support Structure, FS 559.0 to FS 559.0 + 80

(including Floor Beams, Struts, Floor Sills, and Seat RailsDI 48 MO 48 MO

53-41-47-01 Detailed Inspection of the Interior Skin Panels, Frames and Stringers Below Floor, FS 559.0 to FS 559.0 + 80

DI 96 MO 72 MO

53-41-51-01 Detailed Inspection of the Aft Keel Beams In Main Landing Gear (MLG) Wheel Well Area

DI 48 MO 48 MO

53-41-51-02 Detailed Inspection of the Aft Keel Beams Inside the Aft ECS Compartment DI 96 MO 72 MO 53-61-08-01 Detailed Inspection of the Floor Beam Attachments to Rear Pressure Bulkhead DI 48 MO 48 MO

53-61-15-01 Detailed Inspection of the Interior Skin Panels, Frames, and Stringers Below Floor, FS 559.0 + 80 to FS 621.0

DI 48 MO 48 MO

53-61-16-01 Detailed Inspection of the Floor Support Structure, FS 559.0 + 80 to FS 621.0 (Including Floor Edge Members and Seat Rails, but Excluding Attachments to Rear Pressure Bulkhead)

DI24 MO 24 MO

53-61-18-01 Detailed Inspection of the Forward Side of Rear Pressure Bulkhead Below Floor Level

DI 48 MO 48 MO

53-61-20-01 Detailed Inspection of the Cargo Door Cutout Interior Surrounding Structure DI 48 MO 48 MO 53-61-22-01 Detailed Inspection of the Rear Pressure Bulkhead Forward Face Above Floor Level DI 48 MO 48 MO

57-21-01-01 Detailed Inspection of the Forward Face of Center Wing Front Spar Between LBL 50.0 and RBL 50.0

DI 96 MO 72 MO

57-21-04-01 Detailed Inspection of the Aft Face of Center Wing Rear Spar Between LWS 48.0 and RWS 48.0

DI 96 MO 72 MO

57-21-05-01 Detailed Inspection of the Exterior Surface of Center Wing Upper Plank Between LBL 47.0 and RBL 47.0

DI 96 MO 72 MO

57-21-10-01 Detailed Inspection of the Forward Face of Wing Front Spar Between BL 50.0 and WS 389.0

DI 96 MO 72 MO

57-21-28-01 Detailed Inspection of the Main Landing Gear (MLG) Side Brace attach Fitting DI 72 MO 72 MO 57-21-29-01 Detailed Inspection of the Front Spar Bayonet Fitting (Exterior) DI 72 MO 72 MO 57-21-30-01 Detailed Inspection of the Rear Spar Bayonet Fitting (Exterior) DI 72 MO 72 MO 57-21-31-01 Detailed Inspection of the Wing to Fuselage Attach Fitting at FS 424.0 DI 96 MO 72 MO 57-21-32-01 Detailed Inspection of the Wing to Fuselage Attach Fitting at FS473.15 DI 72 MO 72 MO 57-21-33-01 Detailed Inspection of the Wing to Fuselage Attach Fitting at FS513.0 DI 72 MO 72 MO 57-21-38-01 Detailed Inspection of the Lower Wing Plank Access Holes from BL0.0 to

WS314.50, LHS and RHSDI 48 MO 48 MO

Revision 1 / April 15, 2008 Chapter 7: CPCP 2 of 2

Chapter 8: Other Required Maintenance TasksPage i

Revision 1 / April 15, 2008 CRJ200Other Required Maintenance Tasks

IntroductionThe section following contains other required maintenance tasks that are not included in the Bombardier MRM Part 1 or Part 2. Refer to the AD summary for continuouslyupdated information on AD’s.

Format:This manual section is presented in the following format:

• Task Number - Indicates the control number assinged by Chautauqua Airlines, Inc.



• Threshold - Indicates the maximum specified interval for the scheduled task of that item

• Repeat - Identifies the repeat interval for the scheduled task



Maintenance Time Limitations Manual CRJ200 Chapter 8: Other Required Maintenance Items


A/C Weigh CRJ 200 Weighing Procedures FNC 1095 DY 1095 DYCR-25-62-02 GVI AED GVI 500 FH 500 FHAD 2002-03-14 To find and fix cracking of the left and right lower wing

planks, which could result in reduced structural integrity of the wing

DVI 5000 FC ADTask Tracked by RPA task: AD020314

AD 2002-16-02 To prevent failure of key components of the horizontal stabilizer trim actuators (HSTAs), which could result in loss of horizontal trim control and consequent reduced controllability of the airplane

DVI 19200 FH AD

Task Tracked by RPA task: AD021602

AD 2003-09-04 R1 To detect and correct in a timely manner fatigue cracks of the pressure floor skin of the center fuselage at fuselage stations 460 and 513, which could result in failure of the pressure floor skin and consequent rapid decompression of the airplane during flight

DVI 10000FC AD

Task Tracked by RPA task: 030904B

AD 2003-11-11 To prevent failure of the MLG main fittings, which could result in collapse of the MLG upon landing SDI 500 FC AD

eddy current, nitro-gen pressure, strut extension and oil leakage inspection on LH fit-ting. Task Tracked by RPA task: 031111A1

AD 2003-11-11 To prevent failure of the MLG main fittings, which could result in collapse of the MLG upon landing SDI 500 FC AD

eddy current, nitro-gen pressure, strut extension and oil leakage inspection on RH fit-ting. Task Tracked by RPA task: 031111A2

AD 2003-11-11 To prevent failure of the MLG main fittings, which could result in collapse of the MLG upon landing DVI 100FC AD inspection of LH fitting. Task Tracked by RPA task:

031111B1AD 2003-11-11 To prevent failure of the MLG main fittings, which could

result in collapse of the MLG upon landing DVI 100 FC AD inspection of RH fitting. Task Tracked by RPA task: 031111B2

AD 2003-11-20 To prevent temporary loss of braking action due to the freezing of moisture on the input plunger of the brake control valve during steep descent

LUB 1500 FH ADTask Tracked by RPA task: AD031120

AD 2003-20-03 To detect and correct, in a timely manner, fatigue cracks in the vertical beams of the pressure bulkheads at fuselage stations 409+128 and 559, which could result in the reduced structural integrity of the airplane,

DVI 14906 FC 12823 FC AD


AD 2004-10-03 To prevent failure of the engine support beam (ESB), a principal structural element, which could result in reduced structural integrity of the airplane


AD 2004-14-16 AD superceded by AD 2007-03-19AD 2004-14-16 AD superceded by AD 2007-03-19AD 2004-14-16 AD superceded by AD 2007-03-19

Revision 1 / April 15, 2008 Chapter 8: Other Required Maintenance Items 1 of 6



AD 2004-14-16 AD superceded by AD 2007-03-19AD 2004-20-09 AD superceded by AD 2007-01-07AD 2004-20-09 AD superceded by AD 2007-01-07AD 2004-20-09 AD superceded by AD 2007-01-07AD 2004-20-09 AD superceded by AD 2007-01-07AD 2004-22-08 To prevent disconnection of an air supply duct, which, if

combined with failure of a bulkhead check valve, could result in rapid depressurization of the airplane

DVI 4000 FH ADTask Tracked by RPA task: 042208A

AD 2005-03-13 This AD was prompted by reports indicating that the links of the aileron power control unit (PCU) have failed. We are issuing this AD to prevent failure of both links of the aileron PCU, which could result in reduced lateral control of the airplane.

DVI 1000 FH AD


AD 2005-06-04 This AD was prompted by numerous failures of the engine throttle control gearbox, some of which resulted in an in-flight engine shutdown. We are issuing this AD to prevent excessive wear of the gearboxes and subsequent movement or jamming of the engine throttle; movement of the throttle towards the idle position brings it close to the fuel shut-off position, which could result in an in- flight engine shutdown.

DVI 1000 FH AD

LH Throttle quadrant. Task Tracked by RPA task: 050604-1

AD 2005-06-04 This AD was prompted by numerous failures of the engine throttle control gearbox, some of which resulted in an in-flight engine shutdown. We are issuing this AD to prevent excessive wear of the gearboxes and subsequent movement or jamming of the engine throttle; movement of the throttle towards the idle position brings it close to the fuel shut-off position, which could result in an in- flight engine shutdown.

DVI 1000 FH AD

RH Throttle quadrant. Task Tracked by RPA task: 050604-2




AD 2005-10-10 This AD is prompted by a report of a potential failure of the horizontal stabilizer trim actuator (HSTA) secondary nut in conjunction with a latent failure of the HSTA primary load path discovered during sampling program activities. We are issuing this AD to detect and correct latent failure of the primary load path of the HSTA, which, in conjunction with a failure of the HSTA secondary nut, could result in loss of horizontal trim control and consequent reduced controllability of the airplane.

DVI 5000 FH AD


AD 2005-17-12 This AD was prompted by reports of failed wing anti-ice ducts (piccolo tubes) in the leading edge of the wing. We are issuing this AD to prevent cracked piccolo tubes, which could result in air leakage, a possible adverse effect on the anti-ice air distribution pattern and anti-ice capability without annunciation to the flight crew, and consequent reduced controllability of the airplane

SDI 2000 FH AD

Task Tracked by RPA task: 051712-A & 051712-B

AD 2005-17-12 (Terminating Action)

This AD was prompted by reports of failed wing anti-ice ducts (piccolo tubes) in the leading edge of the wing. We are issuing this AD to prevent cracked piccolo tubes, which could result in air leakage, a possible adverse effect on the anti-ice air distribution pattern and anti-ice capability without annunciation to the flight crew, and consequent reduced controllability of the airplane

DIS NOTE NOTE AD

Task Tracked by RPA task: 051712-1 & 051712-2 No Threshold or Repeat - Complete by Date: 06/30/2008

AD 2005-18-06 This AD was prompted by the development of terminating actions for the airplane flight manual (AFM) revisions. We are issuing this AD to prevent aileron control stiffness during flight, which could result in the reduction or possible loss of controllability of the airplane

LUB 6500 FH AD

R22–11–A083–01 - Lubrication of aileron autopilot servo and servo mount engage clutch faces. Task Tracked by RPA task: 051806A





LUB 10500 FH AD

R27–00–A053–01 - Replacement of aileron control pulleys with new or ser-viceable parts. Task Tracked by RPA task: 051806B


LUB 5500 FH AD

R27–11–A082–01 - Lubrication of the aileron control cablesat the wing pulley interfaces. Task Tracked by RPA task: 051806C


LUB 5500 FH AD

R27–11–A082–02 - Lubrication of the aileron rear quadrant and trim lever bearings. Task Tracked by RPA task: 051806D

AD 2005-23-01 This AD results from a fatigue test which revealed cracking of the aft pressure bulkhead; subsequent in-service reports show that fatigue cracking has been found on certain other airplanes. We are issuing this AD to detect and correct cracking in the aft pressure bulkhead, which could result in reduced structural integrity and rapid decompression of the airplane.

DVI NOTE 4360 FC AD

Task Tracked by RPA task: 052301A AD phase-in has precedence over threshold.

AD 2006-05-11 R1 This AD results from a report that the shear pin located in the input lever of two pitch feel simulator (PFS) units failed due to fatigue. We are issuing this AD to prevent undetected failure of the shear pin of both PFS units simultaneously, which could result in loss of pitch feel forces and consequent reduced control of the airplane.

FNC 100 FH AD

R27-31-A024-01. Task Tracked by RPA task: 060511B

AD 2006-10-01 To prevent fluid contamination inside the fire and overheat control unit in the flight compartment, which could result in a false fire alarm and consequent emergency landing. GVI

5000 FH or 24 MO

WCFAD

Task Tracked by RPA task: 061001D

AD 2006-10-06 Relay Inspection and Replacement GVI 5500 FH Task Tracked by RPA task: AD061006




AD 2006-11-09 This AD results from a report that a crack was discovered at the lower forward corner of a cargo door skin cut-out during fatigue testing. We are issuing this AD to detect and correct cracking in the lower forward corner of the cargo door skin cut-out, which could result in reduced structural integrity of the airplane.

DVI 15249 FC 5291 FC AD

AWL 53-61-141. Task Tracked by RPA task: AD061109

AD 2007-01-07 This AD was prompted by a report of a cracked main fitting of the MLG. The FAA is issuing this AD to detect and correct fatigue cracking of the main fitting of the MLG and consequent failure of the main fitting, which could result in the collapse of the MLG

DVI 500 FC AD

LH, (g)(1), (g)(2), (h)(1) and (h)(2). Task Tracked by RPA task: 042009A1


DVI 500 FC AD

RH, (g)(1), (g)(2), (h)(1) and (h)(2). Task Tracked by RPA task: 042009A2


SDI 500 FC 5000 FC AD

LH, (g)(3) and (h)(3). Task Tracked by RPA task: 042009B1


SDI 500 FC 5000 FC AD

RH, (g)(3) and (h)(3). Task Tracked by RPA task: 042009B2


DIS NOTE NOTE AD

Task Tracked by RPA task: AD070107 AD to be Complied with by: 14 MAY 2008

AD 2007-03-19 To detect and correct premature cracking of the main fittings of the MLGs, which could result in failure of the fittings and consequent collapse of the MLGs during landing DVI 100 FC AD

for Par (a) of the AD for the LH MLG fitting. Task Tracked by RPA task: 041416A1




AD 2007-03-19 To detect and correct premature cracking of the main fittings of the MLGs, which could result in failure of the fittings and consequent collapse of the MLGs during landing DVI 100 FC AD

for Par (a) of the AD for the RH MLG fitting. Task Tracked by RPA task: 041416A2

AD 2007-03-19 To detect and correct premature cracking of the main fittings of the MLGs, which could result in failure of the fittings and consequent collapse of the MLGs during landing SDI 500 FC AD

for Par (c) and (e), eddy current and strut inspection of the LH gear. Task Tracked by RPA task: 041416B1

AD 2007-03-19 To detect and correct premature cracking of the main fittings of the MLGs, which could result in failure of the fittings and consequent collapse of the MLGs during landing SDI 500 FC AD

for Par (c) and (e), eddy current and strut inspection of the RH gear. Task Tracked by RPA task: 041416B2

AD 2007-04-24 CRJ Exhaust Tailcone Inspection 1500 FH AD Repetitive Inspection. Task Tracked by RPA task: AD70424A

AD 2007-04-24 CRJ Exhaust Tailcone Bolt Replacement 4000 FH AD Terminating Action. Task Tracked by RPA task: AD70424B

AD 2007-07-07 This AD results from a report that in January 2007, a CF34- 3B1 turbofan engine experienced an uncontained fan disk failure during flight operation. We are issuing this AD to prevent an uncontained fan disk failure and airplane damage.

SDI 5000 FH AD

Task Tracked by RPA task: AD0707-2

AD 2007-15-02 Aileron Backlash DVI 2000 FH 2000 FH AD Task Tracked by RPA task: 071502-AAD 2007-15-02 Aileron PCU Leak Check DVI 5000 FH 5000 FH AD Task Tracked by RPA task: 071502-BAD 2007-15-02 Elevator Backlash DVI 5000 FH 5000 FH AD Task Tracked by RPA task: 071502-CAD 2007-15-02 Rudder Backlash DVI 5000 FH 5000 FH AD Task Tracked by RPA task: 071502-DAD 74-08-09R2 To prevent possible fires that could result from smoking

materials being dropped into lavatory paper or linen waste receptacles

DVI 500 FH ADTask Tracked by RPA task: CRJ A1-A10

AD 2008-06-10 To detect and correct cracking of the frame, whichcould lead to failure of the fuselage structure and possible loss of the airplane.


AD 95-04-05 To prevent the inability of passengers to exit the airplane in the event of an emergency LUB 300 FH AD Task Tracked by RPA task: AD950405


APPENDIXCRJ200

Maintenance Time Limitations Manual

All Rights Reserved. Revision 2 / April 15, 2008

APPENDIX


Revisions to the Maintenance Time Limitations Manual Appendix will be annotated below with Revision date.

Revision No. Revision Date Revision No. Revision Date Revision No. Revision Date

0 December 11,2006 10 20

1 March 1, 2007 11 21

2 April 15, 2008 12 22

3 13 23

4 14 24

5 15 25

6 16 26

7 17 27

8 18 28

9 19 29

ii

Record of Revisions

Appendix


Temporary Revision No. Issue Date Date Inserted Inserted By: Temporary

Revision No. Issue Date Date Inserted Inserted By:

iii

Record of Temporary Revisions

The Manual Holder must record the insertion of Temporary Revisons upon receipt of the Temporary Revision.

APPENDIX


Page No. Revision / Date Page No. Revision / Date Page No. Revision / DateTitle Page Appendix B: Precluded/Deleted 10 2 / April 15, 2008

i 2 / April 15, 2008 i 2 / April 15, 2008 11 2 / April 15, 2008Record of Revisions 1 2 / April 15, 2008 12 2 / April 15, 2008

ii 2 / April 15, 2008 2 2 / April 15, 2008 13 2 / April 15, 2008Record of Temporary Revision 3 2 / April 15, 2008 14 2 / April 15, 2008

iii 2 / April 15, 2008 4 2 / April 15, 2008 15 2 / April 15, 2008List of Effective Pages 5 2 / April 15, 2008 16 2 / April 15, 2008

iv 2 / April 15, 2008 6 2 / April 15, 2008 17 2 / April 15, 2008v 2 / April 15, 2008 7 2 / April 15, 2008 18 2 / April 15, 2008

Revision Highlights 8 2 / April 15, 2008 19 2 / April 15, 20081 2 / April 15, 2008 9 2 / April 15, 2008 20 2 / April 15, 20082 2 / April 15, 2008 10 2 / April 15, 2008 21 2 / April 15, 20083 2 / April 15, 2008 11 2 / April 15, 2008 22 2 / April 15, 20084 2 / April 15, 2008 12 2 / April 15, 2008 23 2 / April 15, 20085 2 / April 15, 2008 13 2 / April 15, 2008 24 2 / April 15, 20086 2 / April 15, 2008 14 2 / April 15, 2008 25 2 / April 15, 20087 2 / April 15, 2008 15 2 / April 15, 2008 26 2 / April 15, 20088 2 / April 15, 2008 16 2 / April 15, 2008 27 2 / April 15, 20089 2 / April 15, 2008 Appendix C: MTL No./Job Card/Check X-Ref 28 2 / April 15, 2008

10 2 / April 15, 2008 i 2 / April 15, 2008 29 2 / April 15, 200811 2 / April 15, 2008 1 2 / April 15, 2008 30 2 / April 15, 200812 2 / April 15, 2008 2 2 / April 15, 2008 31 2 / April 15, 200813 2 / April 15, 2008 3 2 / April 15, 2008 32 2 / April 15, 200814 2 / April 15, 2008 4 2 / April 15, 2008 33 2 / April 15, 2008

Appendix Front Matter 5 2 / April 15, 2008 34 2 / April 15, 2008i 2 / April 15, 2008 6 2 / April 15, 2008 35 2 / April 15, 2008

Appendix A: Other Maintenance Items 7 2 / April 15, 2008 36 2 / April 15, 2008i 2 / April 15, 2008 8 2 / April 15, 2008 37 2 / April 15, 20081 2 / April 15, 2008 9 2 / April 15, 2008 38 2 / April 15, 2008

iv

List of Effective Pages

APPENDIX

Maintenance Time Limitations Manual CRJ200List of Effective Pages

Page No. Revision / Date39 2 / April 15, 200840 2 / April 15, 200841 2 / April 15, 2008

v

Maintenance Time Limitations Manual CRJ200Appendix - Revision Highlights

MTLM No.Revision Description

Appendix

CHQ-24-12-00-02 Added task for reliability. ACHQ-25-50-00-01 Added task for reliability. ACHQ-38-11-01-07 Added for EPA potable water program. A26-22-00-02 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B27-11-05 Task Deleted SEP 14/07 per TR 2B-2126 B27-11-06 Task Deleted SEP 14/07 per TR 2B-2126 B27-15-05-01 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B27-15-05-05 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B27-20-00-03 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B27-21-06 Task Deleted SEP 14/07 per TR 2B-2126 B27-31-00-03 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B27-31-02 Task Deleted SEP 14/07 per TR 2B-2126 B27-34-05-01 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B27-34-05-03 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B27-50-01-07 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B27-50-01-08 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B30-12-12-01 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B30-12-23-01 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B31-41-04-01 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B31-41-04-03 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. B32-00-00-07 Task Deleted R. 11 Part 1 MRM. B33-50-00-03 Task Deleted R. 11 Part 1 MRM. B35-11-03-03 Task moved back into MTLM System/Powerplant section per R. 11 Part 1 MTM. BC27-40-103-01 Task Deleted per TR 2A-32. BR27-31-A024-01 Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-00-061 A Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-11-162 NC Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-21-180 NC-1 Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-21-180 NC-2 Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-21-183 NC-1 Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-21-183 NC-2 Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-21-313 NC-1 Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-21-313 NC-2 Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-31-012 C or D-1 Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-31-012 C or D-2 Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-31-019 NC to C Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-41-010 NC Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-41-057 NC Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-41-067 NC Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-41-102 NC Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-53-41-103 A Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-55-11-061 NC-a Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-55-11-061 NC-b Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-55-21-080 NC-a Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-55-21-080 NC-b Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-55-21-082 NC-a Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-55-21-082 NC-b Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-57-21-037 NC Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-57-21-046 NC Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-57-21-169 NC Task Deleted per Rev. 7 Part 2 MRM. B

Revision 2 / April 15, 2008 Appendix - Revision Highlights 1 of 14



Appendix

REO 601R-57-61-004 B Task Deleted per Rev. 7 Part 2 MRM. BREO 601R-57-61-052 NC Task Deleted per Rev. 7 Part 2 MRM. BAppendix C Front Matter Added Calendar Check Program C21-24-30-03 Revised Check assignment to every A check for reliability purposes. C21-51-13-05 Revised Check assignment to every A check for reliability purposes. C21-51-16-01 Revised Check assignment to every A check for reliability purposes. C21-51-16-03 Revised Check assignment to every A check for reliability purposes. C21-51-21-07 Revised Check assignment to Sep Tracking. C21-51-21-09 Added new task, tracking with 21-51-21-07. C23-71-01-01 Revised from C-Ck program to Calendar Check program C23-71-03-01 Revised from C-Ck program to Calendar Check program C24-32-01-01 FNC to be accomplished via RST task every 1500 FH C24-32-01-03 Revised Task number and JobCard number C24-32-03-01 FNC to be accomplished via RST task every 500 FH C24-32-03-03 Revised Task number and JobCard number C25-61-01-01-A Added New Task C25-61-01-01-B Added New Task C26-14-00-01 Revised JC, broke into two separate LH/RH JC's. C26-14-00-01 Revised JC, broke into two separate LH/RH JC's. C26-22-00-02 Precluded task added back into MTLM. C26-25-00-04 Added new task per R. 11 Part 1 MRM. C27-11-00-07 Revised Check assignment to Sep Tracking. C27-11-00-09 Revised Check assignment to Sep Tracking for AD 2007-15-02 C27-11-05 Task Deleted SEP 14/07 per TR 2B-2126 C27-11-06 Task Deleted SEP 14/07 per TR 2B-2126 C27-15-05-01 Precluded task added back into MTLM. C27-15-05-05 Precluded task added back into MTLM. C27-20-00-03 Precluded task added back into MTLM. C27-20-00-07 Revised Check assignment to Sep Tracking. C27-21-06 Task Deleted SEP 14/07 per TR 2B-2126 C27-31-00-03 Precluded task added back into MTLM. C27-31-02 Task Deleted SEP 14/07 per TR 2B-2126 C27-31-35-03 Revised Check assignment to Sep Tracking. C27-34-05-01 Precluded task added back into MTLM. C27-34-05-03 Precluded task added back into MTLM. C27-42-01 Revised tracking, Life Limit to be tracked in Part Master File in RPA. C27-50-01-03 Revised Check assignment to Sep Tracking. C27-50-01-03 Revised Check assignment to Sep Tracking. C27-50-01-03 Revised Check assignment to Sep Tracking. C27-50-01-03 Revised Check assignment to Sep Tracking. C27-50-01-07 Precluded task added back into MTLM. C27-50-01-08 Precluded task added back into MTLM. C27-51-10 Revised Check assignment to Sep Tracking. Life Limit to be tracked in Part Master File in RPA. C27-53-01a Deleted RPA tracking Number, part effective to this task is not in CHQ system or on CHQ aircraft. C27-53-01b Revised tracking, Life Limit to be tracked in Part Master File in RPA. C27-53-01c Revised tracking, Life Limit to be tracked in Part Master File in RPA. C27-53-05a Deleted RPA tracking Number, part effective to this task is not in CHQ system or on CHQ aircraft. C27-53-05b Deleted RPA tracking Number, part effective to this task is not in CHQ system or on CHQ aircraft. C27-53-05c Revised tracking, Life Limit to be tracked in Part Master File in RPA. C27-53-05d Revised tracking, Life Limit to be tracked in Part Master File in RPA. C




Appendix

27-53-05e Deleted RPA tracking Number, part effective to this task is not in CHQ system or on CHQ aircraft. C27-53-05f Deleted RPA tracking Number, part effective to this task is not in CHQ system or on CHQ aircraft. C27-53-05g Revised tracking, Life Limit to be tracked in Part Master File in RPA. C27-53-05h Revised tracking, Life Limit to be tracked in Part Master File in RPA. C28-11-00-02 Revised from C-Ck program to Calendar Check program C28-11-00-07 Revised from C-Ck program to Calendar Check program C28-11-00-604 Added New Task per TR 2D-4 and added Effectivity per Rev. 7 Part 2 MRM. C28-11-00-604 Added New Task per TR 2D-4 and added Effectivity per Rev. 7 Part 2 MRM. C28-11-00-604 Added New Task per TR 2D-4 and added Effectivity per Rev. 7 Part 2 MRM. C28-12-00-03 Revised from C-Ck program to Calendar Check program C28-21-00-05 Revised from C-Ck program to Calendar Check program C29-11-09-01 Revised Check assignment to Sep Tracking. C29-11-09-01 Revised Check assignment to Sep Tracking. C29-11-40-01 Revised Check assignment to Sep Tracking. C29-11-40-01 Revised Check assignment to Sep Tracking. C29-12-09-01 Revised Check assignment to Sep Tracking. C29-12-36-01 Revised Check assignment to Sep Tracking. C30-12-12-01 Precluded task added back into MTLM. C30-12-23-01 Precluded task added back into MTLM. C31-31-03-01 Revised from C-Ck program to Calendar Check program C31-31-03-09 Revised JobCard number. C31-41-04-01 Precluded task added back into MTLM. C31-41-04-03 Precluded task added back into MTLM. C31-41-04-04 Revised Check assignment to Sep Tracking. C32-00-00-07 Task Deleted R. 11 Part 1 MRM. C32-00-00-20 Revised Check assignment to Sep Tracking. C32-00-00-20 Revised Check assignment to Sep Tracking. C32-00-00-20 Revised Check assignment to Sep Tracking. C32-34-00-01 Revised Check assignment to Sep Tracking. C32-34-00-03 Revised Check assignment to Sep Tracking. C33-50-00-03 Task Deleted R. 11 Part 1 MRM. C33-50-00-05 Added New Task per R. 11 Part 1 MRM. C33-51-04-05 Revised from C-Ck program to Calendar Check program C34-11-00-05 Revised Check assignment. C34-11-00-07 Revised from C-Ck program to Calendar Check program C34-11-01 Revised tracking, Life Limit to be tracked in Part Master File in RPA. C34-13-01-01 Revised from C-Ck program to Calendar Check program C35-11-03-03 Precluded task added back into MTLM. C35-23-07-01 Revised from C-Ck program to Calendar Check program C35-23-07-03 Revised from C-Ck program to Calendar Check program C35-23-07-05 Revised from C-Ck program to Calendar Check program C35-23-13-05 Revised from C-Ck program to Calendar Check program C38-30-01-01 Revised from C-Ck program to Calendar Check program C38-30-01-03 Revised from C-Ck program to Calendar Check program C49-14-19-01 Revised Check Assignment per R. 11 Part 1 MRM. C49-20-00-01 Revised to Separately Tracking. C49-20-01 Revised Task Card Number C49-20-02 Revised Task Card Number C52-11-02-01 Revised from C-Ck program to Calendar Check program C52-11-03-01 Revised from C-Ck program to Calendar Check program C




Appendix

52-11-101a Revised MTL Number C52-11-101b Added New Task C52-11-104a Revised MTL Number C52-11-104b Added New Task C52-11-105 Revised Check Assignment per Rev. 7 Part 2 MRM. C52-11-131 Added New Task per Rev. 7 Part 2 MRM. C52-21-02-01 Revised from C-Ck program to Calendar Check program C52-21-02-01 Revised from C-Ck program to Calendar Check program C52-21-03-01 Revised from C-Ck program to Calendar Check program C52-21-03-01 Revised from C-Ck program to Calendar Check program C52-22-02-01 Revised from C-Ck program to Calendar Check program C52-22-03-01 Revised from C-Ck program to Calendar Check program C52-31-02-01 Revised from C-Ck program to Calendar Check program C52-31-03-01 Revised from C-Ck program to Calendar Check program C52-41-02-01 Revised from C-Ck program to Calendar Check program C52-41-03-01 Revised from C-Ck program to Calendar Check program C52-42-02-01 Revised from C-Ck program to Calendar Check program C52-42-03-01 Revised from C-Ck program to Calendar Check program C53-11-01-01 Revised from C-Ck program to Calendar Check program C53-11-02-01 Revised from C-Ck program to Calendar Check program C53-11-03-01 Revised from C-Ck program to Calendar Check program C53-11-03-01 Revised from C-Ck program to Calendar Check program C53-11-05-01 Revised from C-Ck program to Calendar Check program C53-11-05-01 Revised from C-Ck program to Calendar Check program C53-11-06-01 Revised from C-Ck program to Calendar Check program C53-11-07-01 Revised from C-Ck program to Calendar Check program C53-11-08-01 Revised from C-Ck program to Calendar Check program C53-11-08-01 Revised from C-Ck program to Calendar Check program C53-11-09-01 Revised from C-Ck program to Calendar Check program C53-11-10-01 Revised from C-Ck program to Calendar Check program C53-11-11-01 Revised from C-Ck program to Calendar Check program C53-11-11-02 Revised from C-Ck program to Calendar Check program C53-11-122a Revised Check assignment per Rev. 7 Part 2 MRM. C53-11-122b Added New Task per Rev. 7 Part 2 MRM. C53-11-15-01 Revised from C-Ck program to Calendar Check program C53-11-16-01 Revised from C-Ck program to Calendar Check program C53-11-17-01 Revised from C-Ck program to Calendar Check program C53-11-18-01 Revised from C-Ck program to Calendar Check program C53-11-19-01 Revised from C-Ck program to Calendar Check program C53-21-01-01 Revised from C-Ck program to Calendar Check program C53-21-02-01 Revised from C-Ck program to Calendar Check program C53-21-02-02 Revised from C-Ck program to Calendar Check program C53-21-03-01 Revised from C-Ck program to Calendar Check program C53-21-04-01 Revised from C-Ck program to Calendar Check program C53-21-05-01 Revised from C-Ck program to Calendar Check program C53-21-06-01 Revised from C-Ck program to Calendar Check program C53-21-07-01 Revised from C-Ck program to Calendar Check program C53-21-08-01 Revised from C-Ck program to Calendar Check program C53-21-08-02 Revised from C-Ck program to Calendar Check program C53-21-09-01 Revised from C-Ck program to Calendar Check program C




Appendix

53-21-10-01 Revised from C-Ck program to Calendar Check program C53-21-11-01 Revised from C-Ck program to Calendar Check program C53-21-12-01 Revised from C-Ck program to Calendar Check program C53-21-12-01 Revised from C-Ck program to Calendar Check program C53-21-128 Revised Check assignment per Rev. 7 Part 2 MRM. C53-21-129 Added New Task per Rev. 7 Part 2 MRM. C53-21-13-01 Revised from C-Ck program to Calendar Check program C53-21-13-01 Revised from C-Ck program to Calendar Check program C53-21-14-01 Revised from C-Ck program to Calendar Check program C53-21-17-01 Revised from C-Ck program to Calendar Check program C53-21-18-01 Revised from C-Ck program to Calendar Check program C53-300-06 Revised Check assignment per TR 1-4-1 R. 11 Part 1 MRM. C53-41-01-01 Revised from C-Ck program to Calendar Check program C53-41-02-01 Revised from C-Ck program to Calendar Check program C53-41-02-01 Revised from C-Ck program to Calendar Check program C53-41-03-01 Revised from C-Ck program to Calendar Check program C53-41-03-01 Revised from C-Ck program to Calendar Check program C53-41-04-01 Revised from C-Ck program to Calendar Check program C53-41-07-02 Revised from C-Ck program to Calendar Check program C53-41-08-01 Revised from C-Ck program to Calendar Check program C53-41-09-01 Revised from C-Ck program to Calendar Check program C53-41-10-01 Revised from C-Ck program to Calendar Check program C53-41-10-01 Revised from C-Ck program to Calendar Check program C53-41-109 Revised Check assignment to Sep Tracking C53-41-116 Revised Check assignment to Sep Tracking for AD 2003-20-03 C53-41-12-01 Revised from C-Ck program to Calendar Check program C53-41-12-01 Revised from C-Ck program to Calendar Check program C53-41-138-2 Revised Check assignment per Rev. 7 Part 2 MRM. C53-41-14-01 Revised from C-Ck program to Calendar Check program C53-41-14-01 Revised from C-Ck program to Calendar Check program C53-41-16-01 Revised from C-Ck program to Calendar Check program C53-41-17-01 Revised from C-Ck program to Calendar Check program C53-41-17-01 Revised from C-Ck program to Calendar Check program C53-41-18-01 Revised from C-Ck program to Calendar Check program C53-41-199 Revised Check assignment to Sep Tracking. C53-41-20-01 Revised from C-Ck program to Calendar Check program C53-41-20-01 Revised from C-Ck program to Calendar Check program C53-41-201 Revised Check assignment to Sep Tracking. C53-41-24-01 Revised from C-Ck program to Calendar Check program C53-41-24-01 Revised from C-Ck program to Calendar Check program C53-41-25-01 Revised from C-Ck program to Calendar Check program C53-41-25-01 Revised from C-Ck program to Calendar Check program C53-41-26-01 Revised from C-Ck program to Calendar Check program C53-41-26-01 Revised from C-Ck program to Calendar Check program C53-41-27-01 Revised from C-Ck program to Calendar Check program C53-41-27-01 Revised from C-Ck program to Calendar Check program C53-41-28-01 Revised from C-Ck program to Calendar Check program C53-41-28-01 Revised from C-Ck program to Calendar Check program C53-41-29-01 Revised from C-Ck program to Calendar Check program C53-41-29-01 Revised from C-Ck program to Calendar Check program C




Appendix

53-41-30-01 Revised from C-Ck program to Calendar Check program C53-41-30-01 Revised from C-Ck program to Calendar Check program C53-41-31-01 Revised from C-Ck program to Calendar Check program C53-41-31-01 Revised from C-Ck program to Calendar Check program C53-41-32-01 Revised from C-Ck program to Calendar Check program C53-41-32-01 Revised from C-Ck program to Calendar Check program C53-41-33-01 Revised from C-Ck program to Calendar Check program C53-41-34-01 Revised from C-Ck program to Calendar Check program C53-41-35-01 Revised from C-Ck program to Calendar Check program C53-41-35-01 Revised from C-Ck program to Calendar Check program C53-41-36-01 Revised from C-Ck program to Calendar Check program C53-41-38-01 Revised from C-Ck program to Calendar Check program C53-41-39-01 Revised from C-Ck program to Calendar Check program C53-41-39-01 Revised from C-Ck program to Calendar Check program C53-41-40-01 Revised from C-Ck program to Calendar Check program C53-41-40-01 Revised from C-Ck program to Calendar Check program C53-41-41-01 Revised from C-Ck program to Calendar Check program C53-41-41-01 Revised from C-Ck program to Calendar Check program C53-41-42-01 Revised from C-Ck program to Calendar Check program C53-41-43-01 Revised from C-Ck program to Calendar Check program C53-41-43-01 Revised from C-Ck program to Calendar Check program C53-41-44-01 Revised from C-Ck program to Calendar Check program C53-41-45-01 Revised from C-Ck program to Calendar Check program C53-41-45-01 Revised from C-Ck program to Calendar Check program C53-41-46-01 Revised from C-Ck program to Calendar Check program C53-41-46-01 Revised from C-Ck program to Calendar Check program C53-41-47-01 Revised from C-Ck program to Calendar Check program C53-41-50-01 Revised from C-Ck program to Calendar Check program C53-41-51-01 Revised from C-Ck program to Calendar Check program C53-41-51-02 Revised from C-Ck program to Calendar Check program C53-41-52-01 Revised from C-Ck program to Calendar Check program C53-41-53-01 Revised from C-Ck program to Calendar Check program C53-41-53-01 Revised from C-Ck program to Calendar Check program C53-61-01-01 Revised from C-Ck program to Calendar Check program C53-61-02-01 Revised from C-Ck program to Calendar Check program C53-61-08-01 Revised from C-Ck program to Calendar Check program C53-61-12-01 Revised from C-Ck program to Calendar Check program C53-61-12-01 Revised from C-Ck program to Calendar Check program C53-61-15-01 Revised from C-Ck program to Calendar Check program C53-61-153a Revised Check assignment, this task will not be performed as CHQ has chosen to perform 53-61-153b. C53-61-153b Revised Check assignment to Sep Tracking. C53-61-16-01 Revised from C-Ck program to Calendar Check program C53-61-18-01 Revised from C-Ck program to Calendar Check program C53-61-20-01 Revised from C-Ck program to Calendar Check program C53-61-22-01 Revised from C-Ck program to Calendar Check program C53-61-23-01 Revised from C-Ck program to Calendar Check program C53-61-23-01 Revised from C-Ck program to Calendar Check program C53-61-24-01 Revised from C-Ck program to Calendar Check program C53-61-25-01-1 Revised Check assignment to Sep Tracking, Revised JC. C53-61-25-01-2 Revised Check assignment to Sep Tracking, Revised JC. C




Appendix

53-61-26-01 Revised from C-Ck program to Calendar Check program C53-61-26-01 Revised from C-Ck program to Calendar Check program C53-61-27-01 Revised from C-Ck program to Calendar Check program C53-61-29-01 Revised from C-Ck program to Calendar Check program C53-61-30-01 Revised from C-Ck program to Calendar Check program C53-61-31-01 Revised from C-Ck program to Calendar Check program C53-61-32-01 Revised from C-Ck program to Calendar Check program C53-61-34-01 Revised from C-Ck program to Calendar Check program C53-61-36-01 Revised from C-Ck program to Calendar Check program C53-61-39-01 Revised from C-Ck program to Calendar Check program C53-71-01-01 Revised from C-Ck program to Calendar Check program C53-71-05-01 Revised from C-Ck program to Calendar Check program C53-71-07-01 Revised from C-Ck program to Calendar Check program C53-71-08-01 Revised from C-Ck program to Calendar Check program C53-71-10-01 Revised from C-Ck program to Calendar Check program C53-71-12-01 Revised from C-Ck program to Calendar Check program C54-10-105 Revised Check assignment to CRJ C5 from TBD C54-10-105 Revised Check assignment to CRJ C5 from TBD C54-400-04 Revised Check assignment per Rev. 11 Part 1 MRM. C54-400-08 Revised Check assignment per Rev. 11 Part 1 MRM. C54-51-01-01 Revised from C-Ck program to Calendar Check program C54-51-01-01 Revised from C-Ck program to Calendar Check program C54-51-02-02 Revised from C-Ck program to Calendar Check program C54-51-02-02 Revised from C-Ck program to Calendar Check program C54-51-03-01 Revised from C-Ck program to Calendar Check program C54-51-03-01 Revised from C-Ck program to Calendar Check program C55-11-01-01 Revised from C-Ck program to Calendar Check program C55-11-02-01 Revised from C-Ck program to Calendar Check program C55-11-03-01 Revised from C-Ck program to Calendar Check program C55-11-04-01 Revised from C-Ck program to Calendar Check program C55-11-04-01 Revised from C-Ck program to Calendar Check program C55-11-05-01 Revised from C-Ck program to Calendar Check program C55-11-05-01 Revised from C-Ck program to Calendar Check program C55-11-05-02 Revised from C-Ck program to Calendar Check program C55-11-05-02 Revised from C-Ck program to Calendar Check program C55-11-06-01 Revised from C-Ck program to Calendar Check program C55-11-07-01 Revised from C-Ck program to Calendar Check program C55-11-07-01 Revised from C-Ck program to Calendar Check program C55-11-07-02 Revised from C-Ck program to Calendar Check program C55-11-07-02 Revised from C-Ck program to Calendar Check program C55-11-08-01 Revised from C-Ck program to Calendar Check program C55-11-09-01 Revised from C-Ck program to Calendar Check program C55-11-10-01 Revised from C-Ck program to Calendar Check program C55-11-10-01 Revised from C-Ck program to Calendar Check program C55-11-12-01 Revised from C-Ck program to Calendar Check program C55-11-14-01 Revised from C-Ck program to Calendar Check program C55-11-15-01 Revised from C-Ck program to Calendar Check program C55-11-15-01 Revised from C-Ck program to Calendar Check program C55-11-16-02 Revised from C-Ck program to Calendar Check program C55-11-16-02 Revised from C-Ck program to Calendar Check program C




Appendix

55-11-17-01 Revised from C-Ck program to Calendar Check program C55-11-17-01 Revised from C-Ck program to Calendar Check program C55-11-18-01 Revised from C-Ck program to Calendar Check program C55-11-18-01 Revised from C-Ck program to Calendar Check program C55-11-19-01 Revised from C-Ck program to Calendar Check program C55-11-20-01 Revised from C-Ck program to Calendar Check program C55-11-20-01 Revised from C-Ck program to Calendar Check program C55-11-20-02 Revised from C-Ck program to Calendar Check program C55-11-20-02 Revised from C-Ck program to Calendar Check program C55-11-21-01 Revised from C-Ck program to Calendar Check program C55-11-21-01 Revised from C-Ck program to Calendar Check program C55-11-21-02 Revised from C-Ck program to Calendar Check program C55-11-21-02 Revised from C-Ck program to Calendar Check program C55-21-01-01 Revised from C-Ck program to Calendar Check program C55-21-01-01 Revised from C-Ck program to Calendar Check program C55-21-03-01 Revised from C-Ck program to Calendar Check program C55-21-03-01 Revised from C-Ck program to Calendar Check program C55-21-04-01 Revised from C-Ck program to Calendar Check program C55-21-04-01 Revised from C-Ck program to Calendar Check program C55-21-05-01 Revised from C-Ck program to Calendar Check program C55-21-05-01 Revised from C-Ck program to Calendar Check program C55-21-06-01 Revised from C-Ck program to Calendar Check program C55-21-06-01 Revised from C-Ck program to Calendar Check program C55-21-07-01 Revised from C-Ck program to Calendar Check program C55-21-07-01 Revised from C-Ck program to Calendar Check program C55-300-10 Revised Check assignment per Rev. 11 Part 1 MRM. C55-300-10 Revised Check assignment per Rev. 11 Part 1 MRM. C55-31-01-01 Revised from C-Ck program to Calendar Check program C55-31-02-01 Revised from C-Ck program to Calendar Check program C55-31-03-01 Revised from C-Ck program to Calendar Check program C55-31-05-01 Revised from C-Ck program to Calendar Check program C55-31-08-01 Revised from C-Ck program to Calendar Check program C55-31-09-01 Revised from C-Ck program to Calendar Check program C55-31-10-01 Revised from C-Ck program to Calendar Check program C55-31-11-01 Revised from C-Ck program to Calendar Check program C55-31-12-01 Revised from C-Ck program to Calendar Check program C55-31-13-01 Revised from C-Ck program to Calendar Check program C55-31-14-01 Revised from C-Ck program to Calendar Check program C55-41-02-01 Revised from C-Ck program to Calendar Check program C55-41-03-01 Revised from C-Ck program to Calendar Check program C55-41-04-01 Revised from C-Ck program to Calendar Check program C57-21-01-01 Revised from C-Ck program to Calendar Check program C57-21-02-01 Revised from C-Ck program to Calendar Check program C57-21-02-01 Revised from C-Ck program to Calendar Check program C57-21-03-01 Revised from C-Ck program to Calendar Check program C57-21-03-01 Revised from C-Ck program to Calendar Check program C57-21-04-01 Revised from C-Ck program to Calendar Check program C57-21-05-01 Revised from C-Ck program to Calendar Check program C57-21-05-01 Revised from C-Ck program to Calendar Check program C57-21-06-01 Revised from C-Ck program to Calendar Check program C




Appendix

57-21-07-01 Revised from C-Ck program to Calendar Check program C57-21-07-01 Revised from C-Ck program to Calendar Check program C57-21-08-01 Revised from C-Ck program to Calendar Check program C57-21-08-01 Revised from C-Ck program to Calendar Check program C57-21-09-01 Revised from C-Ck program to Calendar Check program C57-21-09-01 Revised from C-Ck program to Calendar Check program C57-21-10-01 Revised from C-Ck program to Calendar Check program C57-21-10-01 Revised from C-Ck program to Calendar Check program C57-21-11-01 Revised from C-Ck program to Calendar Check program C57-21-11-01 Revised from C-Ck program to Calendar Check program C57-21-12-01 Revised from C-Ck program to Calendar Check program C57-21-12-01 Revised from C-Ck program to Calendar Check program C57-21-13-01 Revised from C-Ck program to Calendar Check program C57-21-13-01 Revised from C-Ck program to Calendar Check program C57-21-14-01 Revised from C-Ck program to Calendar Check program C57-21-14-01 Revised from C-Ck program to Calendar Check program C57-21-150 Revised Check Assignment - task will not be accomplished. C57-21-150 Revised Check Assignment - task will not be accomplished. C57-21-15-01 Revised from C-Ck program to Calendar Check program C57-21-15-01 Revised from C-Ck program to Calendar Check program C57-21-157 Revised to reflect that task is not effective to CHQ aircraft. C57-21-157 Revised to reflect that task is not effective to CHQ aircraft. C57-21-158 Revised to reflect that task is not effective to CHQ aircraft. C57-21-158 Revised to reflect that task is not effective to CHQ aircraft. C57-21-16-01 Revised from C-Ck program to Calendar Check program C57-21-16-01 Revised from C-Ck program to Calendar Check program C57-21-17-01 Revised from C-Ck program to Calendar Check program C57-21-17-01 Revised from C-Ck program to Calendar Check program C57-21-18-01 Revised from C-Ck program to Calendar Check program C57-21-18-01 Revised from C-Ck program to Calendar Check program C57-21-19-01 Revised from C-Ck program to Calendar Check program C57-21-19-01 Revised from C-Ck program to Calendar Check program C57-21-20-01 Revised from C-Ck program to Calendar Check program C57-21-20-01 Revised from C-Ck program to Calendar Check program C57-21-21-01 Revised from C-Ck program to Calendar Check program C57-21-21-01 Revised from C-Ck program to Calendar Check program C57-21-22-01 Revised from C-Ck program to Calendar Check program C57-21-22-01 Revised from C-Ck program to Calendar Check program C57-21-23-01 Revised from C-Ck program to Calendar Check program C57-21-23-01 Revised from C-Ck program to Calendar Check program C57-21-24-01 Revised from C-Ck program to Calendar Check program C57-21-24-01 Revised from C-Ck program to Calendar Check program C57-21-25-01-1 Revised from C-Ck program to Calendar Check program C57-21-25-01-2 Revised from C-Ck program to Calendar Check program C57-21-26-01 Revised from C-Ck program to Calendar Check program C57-21-26-01 Revised from C-Ck program to Calendar Check program C57-21-27-01 Revised from C-Ck program to Calendar Check program C57-21-27-01 Revised from C-Ck program to Calendar Check program C57-21-28-01 Revised from C-Ck program to Calendar Check program C57-21-29-01 Revised from C-Ck program to Calendar Check program C




Appendix

57-21-30-01 Revised from C-Ck program to Calendar Check program C57-21-31-01 Revised from C-Ck program to Calendar Check program C57-21-31-01 Revised from C-Ck program to Calendar Check program C57-21-32-01 Revised from C-Ck program to Calendar Check program C57-21-32-01 Revised from C-Ck program to Calendar Check program C57-21-33-01 Revised from C-Ck program to Calendar Check program C57-21-33-01 Revised from C-Ck program to Calendar Check program C57-21-34-01 Revised from C-Ck program to Calendar Check program C57-21-34-01 Revised from C-Ck program to Calendar Check program C57-21-35-01 Revised from C-Ck program to Calendar Check program C57-21-35-01 Revised from C-Ck program to Calendar Check program C57-21-36-01 Revised from C-Ck program to Calendar Check program C57-21-36-01 Revised from C-Ck program to Calendar Check program C57-21-37-01 Revised from C-Ck program to Calendar Check program C57-21-37-01 Revised from C-Ck program to Calendar Check program C57-21-38-01 Revised from C-Ck program to Calendar Check program C57-21-38-01 Revised from C-Ck program to Calendar Check program C57-31-02-01 Revised from C-Ck program to Calendar Check program C57-31-02-01 Revised from C-Ck program to Calendar Check program C57-51-01-01 Revised from C-Ck program to Calendar Check program C57-51-01-01 Revised from C-Ck program to Calendar Check program C57-51-02-01 Revised from C-Ck program to Calendar Check program C57-51-02-01 Revised from C-Ck program to Calendar Check program C57-51-03-01 Revised from C-Ck program to Calendar Check program C57-51-03-01 Revised from C-Ck program to Calendar Check program C57-51-04-01 Revised from C-Ck program to Calendar Check program C57-51-04-01 Revised from C-Ck program to Calendar Check program C57-51-05-01 Revised from C-Ck program to Calendar Check program C57-51-05-01 Revised from C-Ck program to Calendar Check program C57-52-02-01 Revised from C-Ck program to Calendar Check program C57-52-02-01 Revised from C-Ck program to Calendar Check program C57-52-03-01 Revised from C-Ck program to Calendar Check program C57-52-03-01 Revised from C-Ck program to Calendar Check program C57-52-04-01 Revised from C-Ck program to Calendar Check program C57-52-04-01 Revised from C-Ck program to Calendar Check program C57-52-06-01 Revised from C-Ck program to Calendar Check program C57-52-06-01 Revised from C-Ck program to Calendar Check program C57-52-07-01 Revised from C-Ck program to Calendar Check program C57-52-07-01 Revised from C-Ck program to Calendar Check program C57-52-08-01 Revised from C-Ck program to Calendar Check program C57-52-08-01 Revised from C-Ck program to Calendar Check program C57-52-14-01 Revised from C-Ck program to Calendar Check program C57-52-14-01 Revised from C-Ck program to Calendar Check program C57-52-15-01 Revised from C-Ck program to Calendar Check program C57-52-15-01 Revised from C-Ck program to Calendar Check program C57-52-17-01 Revised from C-Ck program to Calendar Check program C57-52-17-01 Revised from C-Ck program to Calendar Check program C57-52-19-01 Revised from C-Ck program to Calendar Check program C57-52-19-01 Revised from C-Ck program to Calendar Check program C57-52-20-01 Revised from C-Ck program to Calendar Check program C




Appendix

57-52-20-01 Revised from C-Ck program to Calendar Check program C57-53-04-01 Revised from C-Ck program to Calendar Check program C57-53-04-01 Revised from C-Ck program to Calendar Check program C57-53-05-01 Revised from C-Ck program to Calendar Check program C57-53-05-01 Revised from C-Ck program to Calendar Check program C57-53-07-01 Revised from C-Ck program to Calendar Check program C57-53-07-01 Revised from C-Ck program to Calendar Check program C57-53-10-01 Revised from C-Ck program to Calendar Check program C57-53-10-01 Revised from C-Ck program to Calendar Check program C57-53-12-01 Revised from C-Ck program to Calendar Check program C57-53-12-01 Revised from C-Ck program to Calendar Check program C57-53-125 Added New Task per Rev. 7 Part 2 MRM. C57-53-13-01 Revised from C-Ck program to Calendar Check program C57-53-13-01 Revised from C-Ck program to Calendar Check program C57-53-15-01 Revised from C-Ck program to Calendar Check program C57-53-15-01 Revised from C-Ck program to Calendar Check program C57-53-17-01 Revised from C-Ck program to Calendar Check program C57-53-17-01 Revised from C-Ck program to Calendar Check program C57-53-20-01 Revised from C-Ck program to Calendar Check program C57-53-20-01 Revised from C-Ck program to Calendar Check program C57-53-24-01 Revised from C-Ck program to Calendar Check program C57-53-24-01 Revised from C-Ck program to Calendar Check program C57-53-25-01 Revised from C-Ck program to Calendar Check program C57-53-25-01 Revised from C-Ck program to Calendar Check program C57-54-01-01 Revised from C-Ck program to Calendar Check program C57-54-01-01 Revised from C-Ck program to Calendar Check program C57-54-02-01 Revised from C-Ck program to Calendar Check program C57-54-02-01 Revised from C-Ck program to Calendar Check program C57-54-103 Revised Check assignment to Sep Tracking. C57-54-103 Revised Check assignment to Sep Tracking. C57-61-01-01 Revised from C-Ck program to Calendar Check program C57-61-01-01 Revised from C-Ck program to Calendar Check program C57-61-04-01 Revised from C-Ck program to Calendar Check program C57-61-04-01 Revised from C-Ck program to Calendar Check program C57-61-05-01 Revised from C-Ck program to Calendar Check program C57-61-05-01 Revised from C-Ck program to Calendar Check program C57-61-06-01 Revised from C-Ck program to Calendar Check program C57-61-06-01 Revised from C-Ck program to Calendar Check program C57-71-01-01 Revised from C-Ck program to Calendar Check program C57-71-01-01 Revised from C-Ck program to Calendar Check program C57-71-02-01 Revised from C-Ck program to Calendar Check program C57-71-02-01 Revised from C-Ck program to Calendar Check program C57-72-01-01 Revised from C-Ck program to Calendar Check program C57-72-01-01 Revised from C-Ck program to Calendar Check program C57-72-02-01 Revised from C-Ck program to Calendar Check program C57-72-02-01 Revised from C-Ck program to Calendar Check program C57-73-01-01 Revised from C-Ck program to Calendar Check program C57-73-01-01 Revised from C-Ck program to Calendar Check program C57-73-02-01 Revised from C-Ck program to Calendar Check program C57-73-02-01 Revised from C-Ck program to Calendar Check program C




Appendix

57-74-01-01 Revised from C-Ck program to Calendar Check program C57-74-01-01 Revised from C-Ck program to Calendar Check program C71-61-00-07 Added New Task per Rev. 11 Part 1 MRM. C71-61-00-07 Added New Task per Rev. 11 Part 1 MRM. C72-32-00-03 Revised Check assignment to Sep Tracking. C72-32-00-03 Revised Check assignment to Sep Tracking. C72-33-00-01 Revised Check assignment to Sep Tracking. C72-33-00-01 Revised Check assignment to Sep Tracking. C73-11-03-03 Revised Check assignment to better allign with DIS task. C73-11-03-03 Revised Check assignment to better allign with DIS task. C73-21-01-01 Revised Check assignment to Sep Tracking. C73-21-01-01 Revised Check assignment to Sep Tracking. C76-11-00-13 Added New Task per Rev. 11 Part 1 MRM. C78-30-00-03 Revised Check assignment to Sep Tracking. C78-30-00-05 Revised Check assignment to Sep Tracking. C78-30-00-05 Revised Check assignment to Sep Tracking. C79-21-01-01 Revised Check assignment to Sep Tracking. C79-21-01-01 Revised Check assignment to Sep Tracking. C79-21-05-03 Revised Check assignment per R. 11 part 1 MRM. C79-21-05-03 Revised Check assignment per R. 11 part 1 MRM. CAD 2002-16-02 Revised tracking, Life Limit to be tracked in Part Master File in RPA. CAD 2003-20-03 Revised JC number. CAD 2004-10-03 Revised JC number. CAD 2004-14-16 AD superceded by AD 2007-03-19 CAD 2004-14-16 AD superceded by AD 2007-03-19 CAD 2004-14-16 AD superceded by AD 2007-03-19 CAD 2004-14-16 AD superceded by AD 2007-03-19 CAD 2004-20-09 AD superceded by AD 2007-01-07 CAD 2004-20-09 AD superceded by AD 2007-01-07 CAD 2004-20-09 AD superceded by AD 2007-01-07 CAD 2004-20-09 AD superceded by AD 2007-01-07 CAD 2005-17-12 Revised task number and JobCard number CAD 2005-17-12 Revised task number and JobCard number CAD 2005-17-12 Created Terminating Action Task CAD 2005-17-12 Created Terminating Action Task CAD 2005-18-06 Revised JobCard number. CAD 2005-18-06 Revised JobCard number. CAD 2005-18-06 Revised JobCard number. CAD 2005-18-06 Revised JobCard number. CAD 2005-23-01 Revised JobCard number. CAD 2006-10-01 Revised Task number and JobCard number due to change in tracking from A/C to Component CAD 2006-10-01 (Terminating Action) Added Task to cover terminating action requirement. CAD 2006-10-06 Added AD. CAD 2007-01-07 Added New AD, this AD suppercedes AD 2004-20-09. CAD 2007-01-07 Added New AD, this AD suppercedes AD 2004-20-09. CAD 2007-01-07 Added New AD, this AD suppercedes AD 2004-20-09. CAD 2007-01-07 Added New AD, this AD suppercedes AD 2004-20-09. CAD 2007-01-07 (Terminating Action) Added Terminating Action CAD 2007-01-07 (Terminating Action) Added Terminating Action CAD 2007-03-19 Added New AD, this AD suppercedes AD 2004-14-16. C




Appendix

AD 2007-03-19 Added New AD, this AD suppercedes AD 2004-14-16. CAD 2007-03-19 Added New AD, this AD suppercedes AD 2004-14-16. CAD 2007-03-19 Added New AD, this AD suppercedes AD 2004-14-16. CAD 2007-07-07 Added New AD. CAD2007-04-24 Added New AD. CAD2007-04-24 Added New AD. CAD 2008-06-10 Added New AD. CC21-50-115-01 Revised Check assignment per TR 2A-31. CC24-10-129-01 Revised Check assignment to Sep Tracking. CC25-17-152-01 Revised Check assignment per TR 2A-31. CC26-10-131-01 Revised Check assignment per TR 2A-31. CC26-20-131-01 Revised JobCard number. CC27-10-105-01 Revised Check assignment per TR 2A-31. CC27-10-105-01 Revised Check assignment per TR 2A-31. CC27-10-105-03 Revised Check assignment per Rev. 7 Part 2 MRM. CC27-10-105-05a Revised Check assignment to Sep Tracking for AD 2007-15-02 CC27-10-105-05b Revised Check assignment to Sep Tracking for AD 2007-15-02 CC27-10-105-06 Revised Check assignment to Sep Tracking for AD 2007-15-02 CC27-10-105-07 Revised Check assignment per Rev. 7 Part 2 MRM. CC27-10-105-07 Revised Check assignment per Rev. 7 Part 2 MRM. CC27-10-105-07 Revised Check assignment per Rev. 7 Part 2 MRM. CC27-20-108-01 Revised Check assignment per Rev. 7 Part 2 MRM. CC27-30-102-01 Revised Check assignment per Rev. 7 Part 2 MRM. CC27-30-102-03 Revised Check assignment per Rev. 7 Part 2 MRM. CC27-30-102-05 Revised Check assignment per Rev. 7 Part 2 MRM. CC27-30-102-05 Revised Check assignment per Rev. 7 Part 2 MRM. CC27-30-102-05 Revised Check assignment per Rev. 7 Part 2 MRM. CC27-35-112-01 Revised Check assignment per TR 2A-32. CC27-40-103-01 Task Deleted per TR 2A-32. CC27-50-111-01 Revised Check assignment per TR 2A-37. CC27-50-111-01 Revised Check assignment per TR 2A-37. CC27-50-111-03 Revised Check assignment per TR 2A-37. CC27-50-111-03 Revised Check assignment per TR 2A-37. CC27-50-111-06 Revised Check assignment to Sep Tracking. CC27-50-111-06 Revised Check assignment to Sep Tracking. CC27-50-111-06 Revised Check assignment to Sep Tracking. CC27-50-111-06 Revised Check assignment to Sep Tracking. CC27-50-111-07 Revised Check assignment per TR 2A-38. C




Appendix

C27-50-111-07 Revised Check assignment per TR 2A-38. CC27-50-111-07 Revised Check assignment per TR 2A-38. CC27-50-111-07 Revised Check assignment per TR 2A-38. CC27-50-111-10 Revised Check assignment to Sep Tracking CC27-50-111-10 Revised Check assignment to Sep Tracking CC27-50-111-11 Revised Check assignment to Sep Tracking, Revised JC CC27-50-111-11 Revised Check assignment to Sep Tracking, Revised JC CC27-50-111-12 Added New Task per TR 2A-40 Part 2 MRM. Note in check assignment that task is not effective to CHQ fleet. CC27-50-300-01 Added New Task per TR 2A-41 Part 2 MRM. CC27-60-106-01 Revised Check assignment per Rev. 7 Part 2 MRM. CC28-20-131-01 Revised Check assignment per TR 2A-35 CC30-10-141-01 Revised Check assignment to Sep Tracking. CC31-40-158-01 Revised Check assignment per TR 2A-35 CC34-10-141-01 Revised from C-Ck program to Calendar Check program CC34-40-107-01 Revised Check assignment per TR 2A-36 CC35-10-128-01 Revised Check assignment and JC number CC36-20-133-01 Revised Check assignment and JC number CC36-20-133-02 Revised Check assignment and JC number CC52-10-821-01 Revised Check assignment to Sep Tracking. CCHQ-24-12-00-02 New Task created for reliability purpose. CCHQ-25-50-00-01 New Task created for reliability purpose. CCHQ-38-11-01-07 New Task created to comply with EPA Pot Water Program. CR27-31-A024-01 Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-00-061 A Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-11-162 NC Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-21-180 NC-1 Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-21-180 NC-2 Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-21-183 NC-1 Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-21-183 NC-2 Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-21-313 NC-1 Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-21-313 NC-2 Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-31-012 C or D-1 Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-31-012 C or D-2 Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-31-019 NC to C Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-41-010 NC Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-41-057 NC Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-41-067 NC Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-41-102 NC Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-53-41-103 A Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-55-11-061 NC-a Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-55-11-061 NC-b Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-55-21-080 NC-a Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-55-21-080 NC-b Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-55-21-082 NC-a Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-55-21-082 NC-b Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-57-21-037 NC Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-57-21-046 NC Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-57-21-169 NC Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-57-61-004 B Task Deleted per Rev. 7 Part 2 MRM. CREO 601R-57-61-052 NC Task Deleted per Rev. 7 Part 2 MRM. C


Appendix Front MatterPage i

Revision 2 / April 15, 2008 CRJ200

Appendix

IntroductionThe appendix of this manual may be amended and/or revised at the discretion of Chautauqua Airlines, Inc. any time as appropriate, and does not require FAA approvalprior to revision. The Appendix Section is considered as accepted by the FAA, and contains the following sections:

Appendix A: Other Maintenance Items

This part is for any non-required maintenance items that Chautauqua Airlines, Inc. will perform, including Bombardier recommended tasks, Chautauqua Airlines,Inc. implemented tasks, or other manufacturer’s recommended tasks.

Appendix B: Precluded/Deleted Tasks

This part consists of tasks that have been precluded or deleted by another task in the MRM or Chautauqua Airlines, Inc. program due to new tasks that enhanceor improve upon the deleted task.

Appendix C: MTL No./Job Card/Check Cross Reference

This is a list of tasks sorted in ascending order based on the Task Number, Job Card, RPA Misc Task number (where appropriate), Job card Title, and theassociated RPA check package designator. Check packages are: LC1, LC2, CRJ A1 - CRJ A10, CRJ C1 - CRJ C5, CRJ 24 - 120, Separately Tracked Items(SEP), Opportunity Check items (OPP), Sticker Program Items (STKR), To Be Determined (TBD).

Appendix A: Other Maintenance ItemsPage i


Other Maintenance Items

IntroductionThis part is for any non-required maintenance items that Chautauqua Airlines, Inc. will perform, including Bombardier recommended tasks, Chautauqua Airlines,Inc. implemented tasks, or other manufacturer’s recommended tasks.


• Task Number - Indicates the control number assigned by Chautauqua Airlines, Inc.







Maintenance Time Limitations Manual CRJ200Appendix A: Other Maintenance Items

Task Number Task Description Task Threshold Repeat ETOPS/CMR/AD Notes

CHQ-24-12-00-02 Service IDG's SVC 10 Day 10 Day Added for reliability CHQ-25-50-00-01 GVI of the Cargo Restraint Netting GVI 500 FH 500 FH Added for reliability CHQ-38-11-01-07 Potable Water Sampling DVI 12 MO 12 MO Added for EPA potable water program.

Revision 2 / April 15, 2008 Appendix A: Other Maintenance Items 1 of 1

Appendix B: Precluded/DeletedPage i


Precluded/Deleted Tasks

IntroductionThe section following contains the various inspection tasks that have been Precluded or Deleted.









Maintenance Time Limitations Manual CRJ200Appendix B: Precluded/Deleted


21-21-01-01 General Visual Inspection of the Flight Compartment Distribution Ducts and Clamps General Condition and Security

GVI

Note 10 Precluded by Zonal Ref. 53-100-11, 53-100-14, 53-100-17, 53-100-23

21-21-01-03 General Visual Inspection of the Distribution Manifold for General Condition

GVI Note 10 Precluded by Zonal Ref. 53-100-23, 53-100-26

21-21-07-01 Task Deleted Feb 05/9321-22-01-01 General Visual Inspection of the Passenger Cabin

Distribution Ducts and Clamps General Condition and Security

GVI

Precluded by Zonal Ref. 53-100-12, 53-100-15, 53-100-18, 53-100-26

21-22-13-03 Task Deleted Feb 05/9321-24-15-01 General Visual Inspection of the ARINC Cooling

Ducts and Clamps General Condition and SecurityGVI

Note 10 Precluded by Zonal Ref. 53-100-11, 53-100-12

21-24-30-01 General Visual Inspection of the Display Cooling Ducts and Clamps General Condition and Security

GVI


21-51-01-03 Task Deleted Jun 07/9421-51-21-05 Task Deleted Apr 11/0121-51-34-03 General Visual Inspection of the Air Conditioning

Ducts and Clamps General Condition and SecurityGVI

Note 10 Precluded by Zonal Ref. 53-300-02

22-11-00-01 General Visual Inspection of the Yaw Damper Installation for Condition and Security

GVI Note 10 Precluded by Zonal Ref. 55-300-04

22-11-00-05 Task Deleted Apr 11/0122-11-00-07 Task Deleted Apr 11/0122-12-04-01 Task Deleted Dec 15/9522-12-07-01 Task Deleted Dec 15/9523-11-05-01 Task Deleted Oct 04/9923-12-00-01 Task Deleted Apr 11/0123-51-00-01 Task Deleted Apr 11/0123-51-00-09 Task Deleted Jun 07/9423-51-01-01 Task Deleted Apr 11/0123-51-04-01 Task Deleted Apr 11/0123-51-07-01 Task Deleted Apr 11/0123-71-10-01 Task Deleted Apr 11/0124-32-05-01 Task Deleted Dec 15/9525-11-01-01 Task Deleted Jun 30/0425-61-05-01 Task Transferred to MSI 35310125-61-05-03 Task Transferred to MSI 35310125-61-06-01 Task Deleted Jul 08/9325-62-04-01 Task Deleted Apr 11/0126-11-00-01 General Visual Inspection of the Fire and Overheat

Sensing Loops for Condition and SecurityGVI


Revision 2 / April 15, 2008 Appendix B: Precluded/Deleted 1 of 16



26-12-01-01 General Visual Inspection of the Fire and Overheat Sensing Loops In the APU Enclosure for Condition and Security

GVI

Note 10 Precluded by Zonal Ref. 53-300-02

26-21-01-01 Task Deleted Jul 08/9326-21-07-03 Task Deleted Jun 30/0426-21-07-04 Task Deleted Jun 30/0426-21-07-07 Task Deleted Sep 29/9426-21-12-01 Task Deleted Jun 30/0426-21-16-01 Task Deleted Feb 05/9326-22-00-02 Precluded by CMR C26-20-131-0326-22-07-02 Task Deleted Jun 30/0426-22-07-03 Task Deleted Jun 30/0426-22-07-04 Task Deleted Sep 29/9426-25-00-01 Task Deleted Feb 05/9326-25-00-04 Task Deleted Jun 30/0426-25-01-10 Task Deleted May 27/0526-25-01-13 Task Deleted Jun 30/0427-11-00-01 Task Deleted Sep 29/9427-11-05 Discard of the Aileron Control System Input/Output

Unit - Aileron (CFMS)DS Task Deleted SEP 14/07 per TR 2B-2126

27-11-06 Discard of the Aileron Control System Transducer - Aileron Force (CFMS)

DS Task Deleted SEP 14/07 per TR 2B-2126

27-15-01-03 Task Deleted Feb 05/9327-15-05-01 Precluded by CMR C27-10-105-0727-15-05-05 Precluded by CMR C27-10-105-0727-20-00-01 Task Deleted Sep 29/9427-20-00-03 Precluded by CMR C27-10-105-0527-21-06 Discard of the Rudder Control System Transducer -

Rudder Force (CFMS)DS Task Deleted SEP 14/07 per TR 2B-2126

27-31-00-01 Task Deleted Sep 29/9427-31-00-03 Precluded by CMR C27-10-105-0527-31-02 Discard of the Elevator Control System Transducer -

Elevator Force (CFMS)DS Task Deleted SEP 14/07 per TR 2B-2126

27-34-05-01 Precluded by CMR C27-30-102-0527-34-05-03 Precluded by CMR C27-30-102-0527-35-01-03 Task Deleted May 27/0527-40-01-01 Task Deleted Jun 07/9427-40-01-03 Task Deleted May 27/0527-50-01-07 Precluded by CMR C27-50-111-0527-50-01-08 Precluded by CMR C27-50-111-0727-60-01-13 Task Deleted May 27/05




28-11-00-03 General Visual Inspection of the Fuel Lines and Components within Fuel Tanks for Condition and Security of Installation

GVI

Note 10 Precluded by Zonal Task 57-500-02, 57-500-08, 57-500-10, 57-600-02, 57-600-08, 57-600-10

28-13-00-01 General Visual Inspection of the Fuel Transfer System Lines and Main Components for Condition and Security of Installation

GVI

Note 10 Precluded by Zonal Task 57-500-02, 57-500-08, 57-600-02, 57-600-08

28-21-00-01 General Visual Inspection of the Engine Fuel Feed Lines and Components within the Fuel Tanks for Condition and Security of Installation

GVI


28-22-00-01 General Visual Inspection of the Engine Motive Flow Fuel Lines and Main Components within the Fuel Tanks for Condition and Security of Installation

GVI


28-23-00-01 General Visual Inspection of the Standby Fuel Feed System Lines and Components for Condition and Security of Installation

GVI

Note 10 Precluded by Zonal Task 57-500-02, 57-600-02

28-24-00-01 General Visual Inspection of the APU Fuel Feed Lines and Main Components within the Fuel Tanks, Aft Equipment Bay and APU Compartment for Condition and Security of attachment

GVI

Note 10 Precluded by Zonal Task 53-300-02, 57-500-02, 57-500-08, 57-600-02, 57-600-08

28-41-00-01 Task Deleted Jun 07/9428-41-00-03 General Visual Inspection of the Fuel MLI System

Roll and Pitch Ground Attitude Indicators for Condition and Security of Installation

GVI

Note 10 Precluded by Zonal Task 53-200-06

29-11-00-01 Task Deleted Sep 29/9429-11-34-01 Task Deleted Jun 30/0429-12-00-01 Task Deleted Sep 29/9429-12-32-01 Task Deleted Jun 30/0430-12-12-01 Precluded by CMR C30-10-141-0130-12-23-01 Precluded by CMR C30-10-141-0130-22-05-01 General Visual Inspection of the Check Piston Head

of Cowl Anti-Ice Pressure Relief ValvesGVI Note 10 Precluded by Zonal Ref. 71-400-01, 71-400-08

31-21-01-01 Task Deleted Oct 04/9931-31-03-07 Task Deleted Apr 11/0131-41-01-01 Task Deleted Apr 11/0131-41-04-01 Precluded by CMR C31-40-158-0131-41-04-03 Precluded by CMR C31-40-158-0131-41-17-01 Task Deleted Dec 15/9531-41-25-01 Task Deleted Apr 11/0132-00-00-07 Functional Check of the Landing Gear

Extension/Retraction (Normal Operation)Task Deleted R. 11 Part 1 MRM.

32-11-101 Superseded by SSI 32-11-110 and SSI 32-11-111.32-11-103 Superseded by SSI 32-11-112 and SSI 32-11-115.




32-11-109 Merged with SSI 32-11-10832-11-115 Covered by SSI 32-11-11233-50-00-03 Discard of the Emergency Floor Path Lighting

AssmebliesTask Deleted R. 11 Part 1 MRM.

32-50-01-01 Task Deleted Oct 04/9932-50-01-03 General Visual Inspection of the Nose Wheel

Steering Position Feedback AssembliesGVI Refer to

Note Refer to

Note


32-50-01-07 General Visual Inspection of the Nose Wheel Steering Hydraulic Units/Lines for Condition and Security

GVI


33-45-00-01 Task Deleted Oct 04/9933-45-00-03 Task Deleted Oct 04/9934-11-00-03 Task Deleted Oct 04/9934-25-07-01 Task Deleted Apr 11/0134-32-14-01 Task Deleted Oct 04/9934-41-01-01 Task Deleted Apr 11/0134-42-01-01 Task Deleted Dec 15/9534-42-07-01 Task Deleted Oct 04/9934-43-04-01 Task Deleted Oct 04/9934-43-07-01 Task Deleted Oct 04/9934-44-07-01 Task Deleted Oct 04/9934-45-00-03 Task Deleted Oct 04/9934-51-07-01 Task Deleted Oct 04/9934-51-11-01 Task Deleted Oct 04/9934-51-14-01 Task Deleted Oct 04/9934-52-04-01 Task Deleted Oct 04/9934-53-04-01 Task Deleted Oct 04/9934-54-04-01 Task Deleted Oct 04/9935-11-03-03 Precluded by CMR C35-10-128-0135-12-03-01 Task Deleted Jun 30/0435-23-13-01 Task Deleted Apr 11/0135-31-07-01 Task deleted Mar 14/0236-11-31-01 General Visual Inspection of the LH 10th Stage

Bleed Air Ducts and Clamps for General ConditionGVI


36-11-31-03 General Visual Inspection of the RH 10th Stage Bleed Air Ducts and Clamps for General Condition

GVI


36-12-04-01 General Visual Inspection of the LH 14th Stage Bleed Air Ducts and Clamps for General Condition

GVI


36-12-04-03 General Visual Inspection of the RH 14th Stage Bleed Air Ducts and Clamps for General Condition

GVI





38-11-01-03 Task Deleted Oct 04/9938-11-01-05 Task Deleted Oct 04/9938-11-04-01 Task Deleted Oct 04/9938-12-07-01 Task Deleted Oct 04/9938-21-01-03 Task Deleted Oct 04/9938-21-04-01 Task Deleted Oct 04/9938-22-07-01 Task Deleted Oct 04/9938-30-01-05 Task Deleted Feb 05/9349-12-00-03 Task Deleted Oct 04/9949-12-00-05 Task Deleted Oct 04/9949-12-00-07 Task Deleted Oct 04/9949-14-16-01 Task Deleted Feb 05/9349-20-00-05 Task deleted Dec 15/9549-20-00-07 Task deleted Dec 15/9549-20-00-09 Task deleted Dec 15/9549-20-00-11 Task deleted Dec 15/9549-20-00-13 Task deleted Dec 15/9549-20-00-15 Task deleted Dec 15/9549-20-00-19 Task deleted Dec 15/9549-20-00-21 Task deleted Dec 15/9549-20-00-23 Task deleted Dec 15/9549-20-00-25 Task deleted Dec 15/9549-20-00-27 Task deleted Dec 15/9549-24-00-09 Task deleted Dec 15/9549-26-00-03 Task deleted Dec 15/9549-26-00-05 Task deleted Dec 15/9549-31-00-03 Task deleted Dec 15/9549-42-10-03 Task deleted Dec 15/9549-91-00-01 Task deleted Jun 07/9449-91-00-03 Task deleted Dec 15/9549-91-05-01 Task deleted Dec 15/9552-00-00-13 Task Deleted May 27/0552-00-00-15 Task Deleted May 27/0552-11-01-01 General Visual Inspection of the Passenger Door

Exterior SkinGVI 72 Months 72 Months Precluded by Zonal 52-800-05

52-11-01-02 AWL Note 3 Precluded by 52-11-101 and 52-11-10452-11-02-02 AWL Note 3 Precluded by 52-11-102 and 52-11-10552-11-03-02 AWL Note 3 Precluded by 52-11-101 and 52-11-10452-11-103 Incorporated with 52-11-10152-21-01-01 General Visual Inspection of the Overwing

Emergency Exit External SkinGVI 72 Months 72 Months Note 2 Precluded by 52-800-07

52-21-02-02 AWL Note 3 Precluded by 52-11-102 and 52-11-10552-21-03-02 AWL Note 3 Precluded by 52-11-102 and 52-11-10552-21-103 Task Deleted Modsum TC601R25099 Cancelled




52-22-01-01 General Visual Inspection of the Crew Escape Hatch External Skin

GVI 72 Months 72 Months Precluded by 52-800-03

52-22-02-02 AWL Note 3 Precluded by 52-22-10252-22-03-02 AWL Note 3 52-22-10252-31-01-01 General Visual Inspection of the Cargo Door Exterior

SkinGVI 72 Months 72 Months Precluded by 52-800-09

52-31-01-02 AWL Note 3 52-31-10252-31-02-02 AWL Note 3 52-31-10252-31-03-02 AWL Note 3 52-31-10252-41-01-01 General Visual Inspection of the Service Door

Exterior SkinGVI 72 Months 72 Months Precluded by 52-800-11

52-41-02-02 AWL Note 3 52-41-10252-41-03-02 AWL Note 3 Precluded by 52-41-10252-41-103 Incorporated with 52-41-10252-42-01-01 General Visual Inspection of the Avionics

Compartment Door Exterior SkinGVI 72 Months 72 Months Precluded by 52-800-01

52-42-02-02 AWL Note 3 Precluded by 52-42-10352-42-03-02 AWL Note 3 Precluded by 52-42-10352-42-102 Incorporated with 52-42-10353-11-02-02 AWL Note 3 Precluded by 53-11-106 and 53-11-12753-11-02-03 General Visual Inspection of the FS 202.75 forward

Pressure Bulkhead Front FaceGVI 72 Months 72 Months Precluded by 53-100-04, 53-100-05, 53-200-02, and 53-200-03

53-11-03-02 AWL Note 3 Precluded by 53-11-108 and 53-11-11253-11-04-01 Task Deleted Jul 8/9353-11-05-02 AWL Note 3 Precluded by 53-11-12353-11-06-02 Note 3 Precluded by 53-11-11053-11-07-02 AWL Note 3 Precluded by 53-11-11053-11-10-02 AWL Note 3 Precluded by 53-11-10453-11-111 Incorporated with 53-11-11253-11-12-01 General Visual Inspection of the External Skin Below

WL 79.5 (Cockpit Door)GVI 48 Months 48 Months Note 2 Precluded by 53-100-03 and 53-100-07

53-11-12-02 AWL Note 3 Precluded by 53-11-112 and 53-11-12653-11-13-01 General Visual Inspection of the External Skin

Between WL 110.0 and Above WL 79.5GVI 48 Months 48 Months Note 2 Precluded by 53-200-04

53-11-13-02 AWL Note 3 Precluded by 53-11-11253-11-14-01 General Visual Inspection of the Flight Compartment

Exterior SkinGVI 48 Months 48 Months Note 2 Precluded by 53-200-04

53-11-14-02 AWL Note 3 Precluded by 53-11-11053-11-16-02 AWL Note 3 Precluded by 53-11-121 and 53-11-12253-11-17-02 Task Deleted Jul 8/9353-11-18-02 AWL Note 3 Precluded by 53-11-10153-11-19-02 AWL Note 3 Precluded by 53-11-102 and 53-11-10353-11-20-01 General Visual Inspection of the Nose Landing Gear

(NLG) Wheel Well WebGVI 72 Months 72 Months Note 2 Precluded by 53-100-06

53-11-20-02 AWL Note 3 Precluded by 53-11-101




53-21-01-02 AWL Note 3 Precluded by 53-21-10153-21-02-03 AWL Note 3 Precluded by 53-21-10253-21-03-02 AWL Note 3 Precluded by 53-21-10353-21-04-02 Task Deleted Jul 8/9353-21-05-02 Task Deleted Jul 8/9353-21-06-02 Task Deleted Jul 8/9353-21-07-02 AWL Note 3 Precluded by 53-21-10253-21-08-03 AWL Note 3 Precluded by 53-21-10853-21-09-02 AWL Note 3 Precluded by 53-21-11053-21-10-02 AWL Note 3 Precluded by 53-21-11053-21-107 Incorporated with 52-41-10253-21-15-01 General Visual Inspection of the Exterior top Skin

Panels FS 280.0 - FS 409.0, Str 8 to top CenterlineGVI

48 Months 48 Months Note 2 Precluded by 53-200-07 and 53-200-10

53-21-15-02 AWL Note 3 Precluded by 53-21-115 and 53-21-12553-21-16-01 General Visual Inspection of the Exterior Side Skin

Panels from Str 8 to Str 17 (Floor Level)GVI 48 Months 48 Months Note 2 Precluded by 53-200-07 and 53-200-10

53-21-16-02 AWL Note 3 Precluded by 53-21-12553-21-18-02 AWL Note 3 Precluded by 53-21-11853-21-19-01 Task Deleted Jul 8/9353-41-05-01 General Visual Inspection of the Exterior top Skin

Panel FS 409.0 to FS 409 + 129 and Str 6 to Trop Centerline

GVI48 Months 48 Months

Note 2 Precluded by 53-200-10

53-41-05-02 AWL Note 3 Precluded by 53-41-101, 53-41-176, and 53-41-19053-41-06-01 General Visual Inspection of the General Visual

Inspection-Exterior Side Skin Panels FS 409.0 to FS 409.0 + 128 Str 6 to Str 20


Precluded by 53-200-10

53-41-06-02 AWL Note 3 Precluded by 53-41-10353-41-07-01 General Visual Inspection of the General Visual

Inspection -External Lower Skin Panel FS 409.0 to FS 409.0 + 128.0 Str 20 to Bottom Centerline (Area Outside Fairing)

GVI

72 Months 72 Months


53-41-07-03 AWL Note 3 Precluded by 53-41-171 and 53-41-19053-41-08-02 Task Deleted Jul 8/9353-41-09-02 Task Deleted Jul 8/9353-41-102 Incorporated with 53-41-10953-41-106 Incorporated with 53-41-10853-41-11-01 General Visual Inspection of the External Top Skin

Panels FS 409 + 128 to FS 559 Strs 6L to 6RGVI

48 Months 48 Months Note 2 Precluded by 53-200-10

53-41-11-02 AWL Note 3 Precluded by 53-41-107, 53-41-108, 53-41-109, 53-41-110

53-41-113 Incorporated with 53-41-11953-41-114 Incorporated with 53-41-11953-41-115 Superseded by SSI 53-41-177, 53-41-178, and 53-41-179




53-41-117 Incorporated with 53-41-15553-41-118 Incorporated with 53-41-12453-41-121 Incorporated with 53-41-15553-41-122 Incorporated with 53-41-11653-41-123 Incorporated with 53-41-11553-41-13-01 General Visual Inspection of the External Side Skin

Panels FS 409 + 128 to FS 559 Str 6 to Str 17 (Floor Level)



53-41-13-02 AWL Note 3 Precluded by 53-41-111 and 53-41-11253-41-130 Incorporated with 53-41-11053-41-131 Incorporated with 53-41-13953-41-136 Incorporated with 53-41-13953-41-137 Incorporated with 53-41-13953-41-14-02 AWL Note 3 Precluded by 53-41-119 and 53-41-19253-41-140 Incorporated with 53-41-13253-41-147 Incorporated with 53-41-14653-41-148 Incorporated with 53-41-15553-41-15-01 General Visual Inspection of the forward Face of

Frame FS 409 + 128 Below FloorGVI 72 Months 72 Months Precluded by 53-100-14 and 53-100-15

53-41-15-02 AWL Note 3 Precluded by 53-41-116, 53-41-177, 53-41-179, 53-41-184, 53-41-185, and 53-41-188

53-41-151 Incorporated with 53-41-15053-41-152 Incorporated with 53-41-15053-41-154 Incorporated with 53-41-15053-41-16-02 AWL Note 3 Precluded by 53-41-177, 53-41-179, 53-41-188, and 53-41-

18953-41-164 Incorporated with 53-41-10453-41-167 Incorporated with 53-41-10453-41-169 Incorporated with 53-41-12553-41-17-02 AWL Note 3 Precluded by 53-41-120 and 53-41-19153-41-178 Incorporated with 53-41-12453-41-18-02 AWL Note 3 Precluded by 53-41-11653-41-19-01 General Visual Inspection of the forward Face of

Frame FS 559 Below FloorGVI 72 Months 72 Months Precluded by 53-100-19 and 53-100-20

53-41-19-02 AWL Note 3 Precluded by 53-41-12453-41-20-02 AWL Note 3 Precluded by 53-41-12553-41-21-01 General Visual Inspection of the Fuselage Skin

Around Cabin Window CutoutGVI 96 Months 72 Months Precluded by 53-200-10

53-41-21-02 AWL Note 3 Precluded by 53-41-126 and 53-41-18353-41-22-01 AWL Note 3 Precluded by 53-41-12753-41-23-01 AWL Note 3 Precluded by 53-41-12853-41-24-02 AWL Note 3 Precluded by 53-41-16853-41-25-02 AWL Note 3 Precluded by 53-41-132 and 53-41-13953-41-26-02 AWL Note 3 Precluded by 53-41-13353-41-27-02 AWL Note 3 Precluded by 53-41-134




53-41-28-02 AWL Note 3 Precluded by 53-41-13953-41-29-02 AWL Note 3 Precluded by 53-41-13853-41-30-02 AWL Note 3 Precluded by 53-41-13953-41-31-02 Task Deleted Jul 8/9353-41-31-03 AWL Note 3 Precluded by 53-41-141 and 53-41-18253-41-32-02 Task Deleted Jul 8/9353-41-32-03 AWL Note 3 Precluded by 53-41-14253-41-33-02 AWL Note 3 Precluded by 53-41-14553-41-34-02 AWL Note 3 Precluded by 53-41-146, 53-41-149, 53-41-193, 53-41-194,

53-41-19553-41-36-02 AWL Note 3 Precluded by 53-41-15053-41-38-02 AWL Note 3 Precluded by 53-41-155 and 53-41-15653-41-39-02 AWL Note 3 Precluded by 53-41-15753-41-40-02 AWL Note 3 Precluded by 53-41-158, 53-41-159, 53-41-161, 53-41-162,

53-41-16353-41-42-02 AWL Note 3 Precluded by 53-41-10453-41-48-01 General Visual Inspection of the Exterior top Skin

Panel FS 559 to FS 559 + 112 Str 6 to top Centerline


Note 2 Precluded by 53-200-10 and 53-200-30

53-41-48-02 AWL Note 3 Precluded by 53-41-16553-41-49-01 General Visual Inspection of the Exterior Side Skin

Panels FS 559 to FS 559 + 112 Str 6 to 20GVI 96 Months 72 Months Precluded by 53-200-10 and 53-200-30

53-41-49-02 AWL Note 3 Precluded by 53-41-16653-41-51-03 AWL Note 3 Precluded by 53-41-10453-41-52-02 AWL Note 3 Precluded by 53-21-11953-41-53-02 AWL Note 3 Precluded by 53-41-16953-61-01-02 AWL Note 3 Precluded by 53-61-10153-61-02-02 AWL Note 3 Precluded by 53-61-10153-61-03-01 AWL Note 3 Precluded by 53-61-10353-61-04-01 AWL Note 3 Precluded by 53-61-10453-61-05-01 Task Deleted Jul 8/9353-61-05-02 AWL Note 3 Precluded by 53-61-10553-61-06-01 AWL Note 3 Precluded by 53-61-10653-61-07-01 AWL Note 3 Precluded by 53-61-10753-61-09-01 AWL Note 3 Precluded by 53-61-10953-61-10-01 Task Deleted Jul 8/9353-61-10-02 AWL Note 3 Precluded by 53-61-110 and 53-61-14253-61-103 Incorporated with 53-61-11353-61-107 Incorporated with 53-71-10553-61-11-01 AWL Note 3 Precluded by 53-61-11153-61-12-02 AWL Note 3 Precluded by 53-61-11253-61-13-01 AWL Note 3 Precluded by 53-61-11353-61-14-01 AWL Note 3 Precluded by 53-61-11453-61-144 Incorporated with 53-61-11053-61-22-02 AWL Note 3 Precluded by 53-61-147, 53-61-153, and 53-61-154




53-61-25-02 AWL Note 3 Precluded by 53-61-143, 53-61-145, 53-61-146, 53-61-148, 53-61-149, and 53-61-152

53-61-28-01 Task Deleted Jun 30/0453-61-35-01 General Visual Inspection of the Fuselage to

Stabilizer Drag BraceGVI Note 4 Precluded by 53-300-01and 53-300-03

53-61-37-01 General Visual Inspection of the Exterior top Skin Panel FS 559 + 112 to FS 755 Str 6 to top Centerline

GVI

Note 4 Precluded by 53-200-30 and 53-300-01

53-61-38-01 General Visual Inspection of the Exterior Side Skin Panels FS 559 + 112 to FS 755 and Str 6 to Str 20

GVI

Note 4 Precluded by 53-200-30

53-61-40-01 AWL Note 3 Precluded by 53-61-14053-61-41-01 AWL Note 3 Precluded by 53-61-141, 53-61-150 and 53-61-15153-71-01-02 AWL Note 3 Precluded by 53-71-10153-71-02-01 AWL Note 3 Precluded by 53-71-10253-71-03-01 AWL Note 3 Precluded by 53-71-10353-71-04-01 AWL Note 3 Precluded by 53-71-10453-71-05-02 AWL Note 3 53-71-10553-71-06-01 Task Deleted Jul 8/9354-10-100 Task Deleted Oct 05/9654-10-101 TR 2B-2112 Task Deleted May 10/0654-10-102 TR 2B-2112 Task Deleted May 10/0654-51-01-02 AWL Note 3 Precluded by 54-51-10154-51-02-01 General Visual Inspection of the Pylon Box External

SkinsGVI 48 Months 48 Months Precluded by 54-400-01 and 54-400-05

54-51-02-03 AWL Note 3 Precluded by 54-51-10254-51-03-02 AWL Note 3 Precluded by 54-51-10354-51-04-01 General Visual Inspection of the Aft Engine Mount

Support StructureGVI Note 4 Precluded by 54-400-03 and 54-400-07

54-51-04-02 Task Deleted Jul 8/9355-11-01-02 AWL Note 3 Precluded by 55-11-10155-11-02-02 AWL Note 3 Precluded by 55-11-10255-11-03-02 AWL Note 3 Precluded by 55-11-10355-11-04-02 AWL Note 3 Precluded by 55-11-10355-11-05-03 AWL Note 3 Precluded by 55-11-10555-11-06-02 AWL Note 3 Precluded by 55-11-10655-11-07-03 AWL Note 3 Precluded by 55-11-10655-11-08-02 AWL Note 3 Precluded by 55-11-10655-11-09-02 AWL Note 3 Precluded by 55-11-10655-11-10-02 AWL Note 3 Precluded by 55-11-11055-11-101 Incorporated with 55-11-10255-11-104 Incorporated with 55-11-10355-11-107 Incorporated with 55-11-10655-11-108 Incorporated with 55-11-10655-11-109 Incorporated with 55-11-106




55-11-11-01 General Visual Inspection of the Exterior Upper Skin BL6.0 to Tip

GVI 72 Months 72 Months Note 2 Precluded by 55-300-07

55-11-11-02 AWL Note 3 Precluded by 55-11-10555-11-111 Incorporated with 55-11-10555-11-112 Incorporated with 55-11-10655-11-116 Incorporated with 55-11-11555-11-117 Incorporated with 55-11-10555-11-12-02 AWL Note 3 55-11-10655-11-13-01 General Visual Inspection of the Exterior Lower Skin

BL6.0 to TipGVI 48 Months 48 Months Note 2 Precluded by 55-300-07

55-11-15-02 AWL Note 3 Precluded by 55-11-11555-11-16-01 Task Deleted Jul 8/9355-11-16-03 AWL Note 3 Precluded by 55-11-11555-11-17-02 AWL Note 3 Precluded by 55-11-11555-11-18-02 Task Deleted Jul 8/9355-11-19-02 AWL Note 3 Precluded by 55-11-11955-11-20-03 Task Deleted Jul 8/9355-21-01-02 AWL Note 3 Precluded by 55-21-10155-21-02-01 General Visual Inspection of the Elevator Skins GVI 72 Months 72 Months Note 2 Precluded by 55-300-0755-21-02-02 AWL Note 3 Precluded by 55-21-10155-21-03-02 AWL Note 3 Precluded by 55-11-11555-21-04-02 AWL Note 3 Precluded by 55-11-115 and 55-21-10755-21-05-02 AWL Note 3 Precluded by 55-11-115 and 55-21-10755-21-06-02 AWL Note 3 Precluded by 55-21-10155-21-102 Incorporated with 55-21-10155-21-103 Incorporated with 55-11-11555-21-104 Incorporated with 55-11-11555-21-105 Incorporated with 55-11-11555-21-106 Incorporated with 55-21-10155-300-06 General Visual Inspection of the Internal Rudder

Assembly Note 1

55-300-11 General Visual Inspection of the Internal LH and RH Elevators Note 1

55-31-01-02 AWL Note 3 Precluded by 55-31-10155-31-02-02 AWL Note 3 Precluded by 55-31-10255-31-04-01 AWL Note 3 Precluded by 55-31-10455-31-06-01 Task Deleted Jul 8/9355-31-07-01 General Visual Inspection of the Vertical Stabilizer

Exterior SkinsGVI Note 4 Precluded by 55-300-01

55-31-08-02 AWL Note 3 Precluded by 55-31-10855-31-09-02 Task Deleted Jul 8/9355-31-11-02 Note 3 Precluded by 55-31-11155-31-12-02 AWL Note 3 Precluded by 55-31-11255-41-01-01 General Visual Inspection of the Rudder Exterior GVI Note 4 Precluded by 55-300-0157-21-01-02 AWL Note 3 Precluded by 57-21-114 and 57-21-118




57-21-04-02 AWL Note 3 Precluded by 57-21-10757-21-06-02 AWL Note 3 Precluded by 57-21-112, 57-21-116, and 57-21-11757-21-10-02 AWL Note 3 Precluded by 57-21-11057-21-104 Superseded by SSI 57-21-146, 57-21-147, 57-21-148, and 57-21-

149.57-21-106 Incorporated with 57-21-11257-21-109 Incorporated with 57-21-11257-21-126 Incorporated with 57-21-13057-21-13-02 AWL Note 3 Precluded by 57-21-111, 57-21-135, 57-21-136, 57-21-151,

and 57-21-15357-21-137 Incorporated with 57-12-13857-21-144 Incorporated with 57-12-11557-21-15-02 Task Deleted Jul 08/9357-21-16-02 AWL Note 3 Precluded by 57-21-139 and 57-21-14057-21-17-02 AWL Note 3 Precluded by 57-21-124, 57-21-125, and 57-21-13457-21-19-02 AWL Note 3 Precluded by 57-21-14257-21-20-02 AWL

Note 3 Precluded by 57-21-101, 57-21-103, 57-21-104, 57-21-105, 57-21-106, 57-21-109, 57-21-113, 57-21-115, 57-21-141, 57-21-146, 57-21-147, 57-21-148, 57-21-149, 57-21-150, 57-21-151, 57-21-152, 57-21-153, and 57-21-154

57-21-20-03 Task Deleted Jul 08/9357-21-22-02 Task Deleted Jul 08/9357-21-24-02 Task Deleted Jul 08/9357-21-25-02 AWL Note 3 Precluded by 57-21-128 and 57-21-13057-21-26-02 Task Deleted Jul 08/9357-21-26-03 AWL Note 3 Precluded by 57-21-145 and 57-21-15557-21-27-02 Task Deleted Jul 08/9357-21-28-02 AWL Note 3 Precluded by 57-21-12057-21-31-02 AWL Note 3 Precluded by 57-21-12257-21-32-02 AWL Note 3 Precluded by 57-21-12357-21-33-02 AWL Note 3 Precluded by 57-21-11957-21-34-02 AWL Note 3 Precluded by 57-21-12157-21-35-02 AWL Note 3 Precluded by 57-21-12757-31-01-01 AWL Note 3 Precluded by 57-21-13857-500-19 General Visual Inspection of the Internal LH Inboard

Flap Note 1

57-51-05-02 AWL Note 3 Precluded by 57-21-14357-52-01-01 General Visual Inspection of the Inboard Flap Upper

Skin - ExteriorGVI 48 Months 48 Months Note 2 Precluded by 57-500-16 and 57-600-16

57-52-01-02 AWL Note 3 Precluded by 57-52-11257-52-02-02 AWL Note 3 Precluded by 57-52-11257-52-03-02 AWL Note 3 Precluded by 57-52-10557-52-05-01 AWL Note 3 Precluded by 57-52-10557-52-06-02 AWL Note 3 Precluded by 57-52-10657-52-07-02 AWL Note 3 Precluded by 57-52-107




57-52-08-02 AWL Note 3 Precluded by 57-52-108 and 57-52-11357-52-101 Incorporated with 57-52-11257-52-102 Incorporated with 57-52-11257-52-103 Incorporated with 57-52-10557-52-111 Incorporated with 57-52-10857-52-115 Superseded by 27-54-15 (Life item)57-52-117 Incorporated with 57-52-11857-52-120 Superseded by 27-54-15 (Life item)57-52-14-02 AWL Life Item, Precluded by 27-54-1557-52-15-02 AWL Life Item, Precluded by 27-54-1557-52-17-02 AWL Note 3 Precluded by 57-52-11857-52-19-02 AWL Note 3 Precluded by 57-52-11957-53-01-01 General Visual Inspection of the Outboard Flap

Upper Skin ExteriorGVI 48 Months 48 Months Note 2 Precluded by 57-500-21 and 57-600-21

57-53-01-02 AWL Note 3 Precluded by 57-53-10257-53-02-01 General Visual Inspection of the Outboard Flap

Lower Skin ExteriorGVI 72 Months 72 Months Precluded by 57-500-21 and 57-600-21

57-53-02-02 AWL Note 3 Precluded by 57-53-10257-53-03-01 AWL Note 3 Precluded by 57-53-10357-53-04-02 AWL Note 3 Precluded by 57-53-104 and 57-53-10757-53-05-02 AWL Note 3 Precluded by 57-53-10657-53-07-02 AWL Note 3 Precluded by 57-53-11457-53-10-02 AWL Note 3 Precluded by 57-53-11457-53-101 Incorporated with 57-53-10257-53-108 Incorporated with 57-53-11457-53-109 Incorporated with 57-53-10757-53-111 Incorporated with 57-53-11457-53-113 Incorporated with 57-53-10657-53-116 Incorporated with 57-53-10657-53-117 Incorporated with 57-53-10757-53-119 Incorporated with 57-53-11857-53-12-02 AWL Note 3 Precluded by 57-53-106 and 57-53-11457-53-120 Incorporated with 57-53-11057-53-123 Incorporated with 57-53-12257-53-13-02 AWL Note 3 Precluded by 57-53-11457-53-15-02 AWL Note 3 Precluded by 57-53-10657-53-17-02 AWL Note 3 Precluded by 57-53-11457-53-20-02 AWL Note 3 Precluded by 57-53-11457-53-22-01 General Visual Inspection of the Outboard Flap

Vane Skins ExteriorGVI 96 Months 72 Months Precluded by 57-500-21 and 57-600-21

57-53-22-02 AWL Note 3 Precluded by 57-53-12257-53-24-02 AWL Note 3 Precluded by 57-53-12257-53-25-02 AWL Note 3 Precluded by 57-53-11057-54-01-02 AWL Note 3 Precluded by 57-54-10357-54-02-02 AWL Note 3 Precluded by 57-54-105




57-600-19 General Visual Inspection of the Internal RH Inboard Flap Note 1

57-61-01-02 AWL Note 3 Precluded by 57-61-101 and 57-61-10657-61-02-01 General Visual Inspection of the Aileron Lower Skin

ExteriorGVI 96 Months 72 Months Precluded by 57-500-21 and 57-600-21

57-61-02-02 AWL Note 3 Precluded by 57-61-102 and 57-61-10757-61-03-01 General Visual Inspection of the Aileron Upper Skin

ExteriorGVI 48 Months 48 Months Note 2 Precluded by 57-500-21 and 57-600-21

57-61-03-02 AWL Note 3 Precluded by 57-61-102 and 57-61-10757-61-04-02 AWL Note 3 Precluded by 57-61-104 and 57-61-10857-61-05-02 AWL Note 3 Precluded by 57-61-10557-61-06-02 AWL Note 3 Precluded by 57-61-10971-12-00-01 General Visual Inspection of the Core Cowl Doors,

Hinges and Latches for Condition and Security of Installation

GVI

Note 10 Precluded by Zonal Tasks 71-400-01 and 71-400-08

71-13-00-01 General Visual Inspection of the Entrance to IDG Oil Cooler to Detect Blockage and of the Engine Service Pylon for Condition and Security of Installation

GVI


71-15-00-01 General Visual Inspection of the Engine Exhaust Nozzle Fairings and Access Panels for Condition and Security of Installation

GVI


71-16-00-01 General Visual Inspection of the Engine forward Core Cowl for Condition and Security of Installation

GVI


71-16-00-05 Task Deleted Jun 30/0471-16-00-11 Task Deleted Jun 30/0471-22-101 Task Deleted Oct 05/9671-51-00-01 General Visual Inspection of the Powerplant Core

Cowl Master Harness A (Red)GVI Note 10 Precluded by Zonal task 71-400-06 and 71-400-13

71-51-00-03 General Visual Inspection of the Powerplant Core Cowl Master Harness B (Violet)

GVI Note 10 Precluded by Zonal Tasks 71-400-06 and 71-400-13

71-52-00-01 General Visual Inspection of the Powerplant Nose Cowl Accessories Harness (orange)

GVI Note 10 Precluded by Zonal Tasks 71-400-06 and 71-400-13

71-61-00-03 Task Deleted Jun 30/0472-32-00-09 General Visual Inspection of the Exposed Area of

the Exterior of the Engine Compressor Case for Condition and Security

GVI


72-32-00-11 Task Deleted Dec 15/9572-41-00-05 Task Deleted Apr 30/9672-51-00-01 Task Deleted Nov 20/9773-11-06-01 Task Deleted Jul 08/9373-21-01-05 General Visual Inspection of the Engine BLUE

ELECTRICAL CABLE (W2) for Condition and Security

GVI





73-21-01-07 General Visual Inspection of the Engine YELLOW ELECTRICAL CABLE (W8) for Condition and Security

GVI


75-30-00-01 General Visual Inspection of the Engine Variable Geometry Actuators for Security at Attachment Points

GVI

Note 10 Precluded by Zonal Task 71-400-06 and 71-400-13

75-30-00-03 General Visual Inspection of the Variable Geometry Feedback Cable for Damage and Attachment

GVI


76-11-00-07 General Visual Inspection of the Throttle Gear Box Mounting Box Bracket for Condition and Security of Installation

GVI


78-30-00-01 Task Deleted Apr 11/0179-12-00-03 General Visual Inspection of the Oil Replenishment

System and Related Components for Condition and Security of Installation

GVI


79-21-07-01 Task Deleted Dec 15/95C27-40-103-01 Removal of the HSTA, Off-Aircraft Inspection for

Structural Integrity and Function of the Mechanical Slip Clutches (Overhaul)

Task Deleted per TR 2A-32.

C34-10-141-02 Task DeletedR27-31-A024-01 Functional Check of the Pitch Feel Simulator (PFS)

Pilot Input LeverTask Deleted per Rev. 7 Part 2 MRM.

R49-14-237-01 Task DeletedR49-20-241-01 Task DeletedR52-30-205-01 Task DeletedREO 601R-53-00-061 A Generic Rpr to Fuse Skin Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-11-162 NC Fastener Hole Fwd Fuse Access Panel Door Doub Task Deleted per Rev. 7 Part 2 MRM.

REO 601R-53-21-180 NC-1 Repair to Fuse Skin Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-21-180 NC-2 Repair to Fuse Skin Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-21-183 NC-1 Repair to Fuse Skin Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-21-183 NC-2 Repair to Fuse Skin Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-21-313 NC-1 Repair to Fuse Skin Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-21-313 NC-2 Repair to Fuse Skin Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-31-012 C or D-1 Deviation-REO 601R-51-31-012 (SB 601R-53-046) Task Deleted per Rev. 7 Part 2 MRM.

REO 601R-53-31-012 C or D-2 Deviation-REO 601R-51-31-012 (SB 601R-53-046) Task Deleted per Rev. 7 Part 2 MRM.

REO 601R-53-31-019 NC to C Repair to Pressure Bulkhead, FS 409.00 + 128 Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-41-010 NC Instal Oversixed Bush Fuse to Wing Pick Up Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-41-056 NC, A, B, C Damage Tolerance Assessment has Established

that No Special Inspections are Required for this Repair

DVI

TR 2B-2115 Note: Inspection of this repair is covered by AWL 53-41-116.




REO 601R-53-41-057 NC Repair to Press Bulkhead Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-41-067 NC Repair to Bulkhead Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-41-102 NC Repair to Pressure Floor Skin, FS 460.00 Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-41-103 A Temp Repair to Press Floor Web Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-61-269 NC, A Damage Tolerance Assessment has Established

that No Special Inspections are Required for this Repair

DVI

TR 2B-2116 Inspection of this repair is covered by Zonal 53-300-01 and 53-300-02.


Appendix C: MTL No./Job Card/Check Cross ReferencePage i


Appendix C: MTL No./Job Card/Check Cross Reference

IntroductionThis is a list of tasks sorted in ascending order based on the task number, and shows the associated Task Description, Job Card, RPA Misc Task number (whereappropriate), and the associated check package.


• MTL Number - Indicates the control number assigned by either the MRM or Chautauqua Airlines, Inc.

• Task Card - Indicates the associated Task card to MTL task.

• RPA Task No. - Indicates the task code used in RPA for items that are separately tracked.


• Check Type - Indicated with an “X” in correlation with the check that the task is assigned to be accomplished.

• LC1 - Line Check 1

• LC2 - Line Check 2

• CRJ A1 - A10 - A check program

• CRJ C1 - C5 - C Check program

• CRJ 24 - 120 - Calendar Check program

• SEP - Separately Tracked item

• OPP - Opportunity Check item

• STKR - Item accomplished via Sticker program

• TBD - Check to be determined


Appendix C: MTL No./Job Card/Check Cross Reference MTL No Task Card RPA Task No. Title LC1 LC2 CRJ

A1CRJ A2

CRJ A3

CRJ A4

CRJ A5

CRJ A6

CRJ A7

CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672

CRJ 120 SEP OPP STKR TBD

21-24-30-03 000-21-220-002 DIS Cockpit-Display Cooling Air-Filter X X X X X X X X X X21-25-01-01 000-21-280-120 GVI Class "C" Cargo Pit Ducts and Clamps X21-31-10-01 000-21-900-101 OPC Cabin Pressure-Control System X21-31-13-01 000-21-140-001 OPC Cabin Pressure Controllers X X X X X21-32-01-01 000-21-170-100 DIS Primary Outflow-Valve Air-Filter X21-32-01-02 000-21-170-101 Clean Primary and Secondary Outflow Valves X21-32-04-01 000-21-170-101 Clean Primary and Secondary Outflow Valves X21-51-00-01 000-21-900-102 OPC Air Conditioning Overpressure Circuit X21-51-04-01 000-21-310-704 B2151001 RST Precoolers by Cleaning X21-51-13-01 LC2 DVI Air Cycle Machine (ACM) Oil Level X21-51-13-05 000-21-310-706 DIS Air-Cycle-Machine Oil X X X X X X X X X X21-51-13-09 000-21-310-707 B2151002 RST Dual Heat Exchanger (Core) X21-51-16-01 000-21-310-003 Clean Water Separator Coalescers X X X X X X X X X X21-51-16-03 000-21-310-004 OPC Water Separator Overboard-Drain Line X X X X X X X X X X21-51-21-07 000-21-170-700 B0520002 DVI Pressure Bulkhead Check Valve X21-51-21-09 000-21-170-700 B0520002 DVI Pressure Bulkhead Check Valve X21-52-10-01 000-21-220-101 OPC Ram Air Shut-Off Valve X21-55-07-01 000-21-900-100 OPC Cargo Compartment Air Shut-Off Valves X21-55-07-03 000-21-900-100 OPC Cargo Compartment Air Shut-Off Valves X21-55-07-05 000-21-900-100 OPC Cargo Compartment Air Shut-Off Valves X22-11-00-03 000-22-160-140 FNC Aileron Servo-Mount Clutch Torque Setting X

22-11-00-03 000-22-320-140 FNC Elevator Servo-Mount Clutch Torque Set X22-11-00-09 000-12-160-701 LUB Aileron Servo Clutch X22-11-00-09 000-12-320-700 LUB Elevator Servo Clutch X23-31-13-01 000-23-900-100 FNC Cabin Speaker/Auto Vol Increase/PA Over'd X

23-51-00-03 000-23-220-101 OPC Crew Oxygen-Mask Microphone X23-51-00-05 000-23-220-101 OPC Crew Oxygen-Mask Microphone X23-51-00-07 000-23-220-101 OPC Crew Oxygen-Mask Microphone X23-51-01-03 000-23-220-122 OPC Audio Control Panel RT & EMER/NORM

Switch X

23-61-00-01 000-23-900-120 Bonding and Megger Test Static Dischargers X23-71-01-01 000-23-900-730 FNC CVR for Intelligibility X23-71-03-01 000-23-360-720 FNC CVR Underwater Locator Device X23-71-03-03 000-23-360-760 RST CVR Underwater Locator Device X X X X X X X X X X23-82-01-01 000-23-220-121 OPC Standby Tuning System (CTL 23) X24-12-00-01 000-24-430-001 VCK LH Eng IDG Filter Indicators X X X X X X X X X X24-12-00-01 000-24-440-001 VCK RH Eng IDG Filter Indicators X X X X X X X X X X24-12-00-02 000-12-430-003 SVC LH Eng IDG Oil X X X X X X X X X X24-12-00-02 000-12-440-003 SVC RH Eng IDG Oil X X X X X X X X X X24-12-00-03 000-24-430-002 DIS LH Eng IDG Oil/Charge and Scav Filters X X X X X24-12-00-03 000-24-440-002 DIS RH Eng IDG Oil/Charge and Scav Filters X X X X X24-12-00-05 000-24-900-100 FNC IDG Disconnect System X24-20-00-01 000-24-220-101 FNC AC Power-Transfer Circuit X24-23-11-01 000-24-220-701 B2423002 FNC (In-Flight Deployment) ADG X24-23-11-01 000-24-900-702 B2423002 FNC (On Ground) Dry ADG X24-23-11-03 000-24-220-701 B2423002 FNC (In-Flight Deployment) ADG X24-23-11-03 000-24-900-702 B2423002 FNC (On Ground) Dry ADG X24-23-11-05 000-24-900-750 B2423001 DIS ADG Uplock Mechanism Cartridge X24-23-11-07 000-12-120-701 B2423002 LUB Air Driven Generator (ADG) Pivot Shaft X24-23-11-07 000-12-120-702 B2423002 LUB Air Driven Generator (ADG) Pivot Shaft X24-30-00-01 000-24-220-100 OPC Essential TRU 1 and TRU 2 X24-30-00-03 000-24-220-001 FNC DC Power Distribution X X X X X24-30-00-05 000-24-220-102 OPC DC Power-Transfer Circuit X24-30-00-07 000-24-900-102 OPC Battery Circuitry X

Revision 2 / April 15, 2008 Appendix C: MTL No./JC/Check X-Reference 1 of 41



A1CRJ A2

CRJ A3

CRJ A4

CRJ A5

CRJ A6

CRJ A7

CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


24-30-00-09 000-24-210-100 OPC TRU Fans X24-32-01-01 000-24-310-001 B2432001 FNC Main Battery X24-32-01-03 000-24-310-001 B2432001 RST Main Battery X24-32-03-01 000-24-310-002 B2432003 FNC APU Battery X24-32-03-03 000-24-310-002 B2432003 RST APU Battery X24-32-07-01 000-24-900-700 B0520001 OPC Main and APU Battery Controllers X25-11-01-03 000-25-220-101 DVI Flight Compt Seats X25-11-01-05 000-25-220-104 DVI Flight Compt Seat Belts/Harnesses X25-11-01-07 000-25-220-102 OPC Flight Compt Seats Inertia Reel X25-17-01-01 000-25-220-701 FNC Cockpit Door Decompression Latch X25-17-01-02 000-25-220-001 DVI Cockpit Door Decompression Latch X X X X X25-17-01-03 000-25-220-105 OPC Cockpit Door Quick Release Hinges X25-21-01-01 000-25-900-102 FNC Pax Seat Breakover Mechanism X25-21-01-03 000-25-900-103 DVI LH Side PAX Seat Locks and Seat Structure X

25-21-01-03 000-25-900-104 DVI RH Side PAX Seat Locks and Seat Structure X

25-21-02-01 000-25-900-106 DVI LH Side PAX Seat Belts X25-21-02-01 000-25-900-107 DVI RH Side PAX Seat Belts X25-22-01-01 000-25-900-108 DVI Flight Attendant Seat/Attachment X25-22-01-03 000-25-900-108 DVI Flight Attendant Seat/Attachment X25-22-02-01 000-25-900-105 DVI Flight Attendant’s Seat Harness X25-40-00-01 000-25-270-001 DVI Lavatory Waste Compartment X X X25-61-01-01 LC2 FNC Life Vests (Shop) X25-61-01-01-A LC2 GVI Life Vest X25-61-01-01-B LC2 RST Life Vest X25-61-02-01 LC2 Operational check of the Flashlights X25-61-03-01 LC2 DVI first aid & emerg med kit for cond & seal X25-61-04-01 000-25-900-700 B0520001 Inspect Emergency Equipment X25-62-01-01 000-25-360-720 E2561961 DIS ELT Battery X25-62-01-03 000-25-220-700 E256171B OPC Emergency Locator Transmitter (ELT) X25-63-01-01 000-25-900-700 B0520001 Inspect Emergency Equipment X26-11-00-02 000-26-430-001 GVI LH ENG Jet-Pipe Sensing Loop X X X X X X X X X X26-11-00-02 000-26-440-001 GVI RH ENG Jet-Pipe Sensing Loop X X X X X X X X X X26-14-00-01 000-26-160-100-1 GVI LH MLG Wheel Well Oheat Detection

System X

26-14-00-01 000-26-160-100-2 GVI RH MLG Wheel Well Oheat Detection System

26-14-01-01 000-26-900-704 FNC MLG Wheel-Well Detector-Loops X26-15-00-01 000-26-900-001 RST (Clean) Cargo Compt Smoke Detectors X X26-16-00-01 000-26-280-700 B0520001 OPC Lavatory Smoke Detector X26-21-01-03 LC2 OPC Eng Firex Sys Switch/Lights X26-21-04-01 000-26-900-150 FNC BOTTLE PUSH TO DISCH Switch/Lights X26-21-07-01 000-26-310-001 VCK Eng and APU Fire EXT Bottle Pressure X X X X X26-21-07-06 000-26-310-750 B2621001 HYDRO CK Eng Fire Extinguisher Bottles X26-21-10-01-1 000-26-310-760 B2621002 DIS Eng Fire Extinguisher Cartridges X26-21-10-01-2 000-26-310-760 DIS Eng Fire Extinguisher Cartridges X26-21-16-03 000-26-900-120 DVI Eng Fire Extinguishing System Lines X26-22-00-01 000-26-900-703 FNC APU Fire-Extinguishing System X26-22-00-0226-22-00-03 000-26-900-141 FNC APU Extinguishing Unattended Mode X26-22-07-01 000-26-310-001 VCK Eng and APU Fire EXT Bottle Pressure X X X X X26-22-07-06 000-26-310-751 B2622001 HYDRO CK APU Fire Extinguisher Bottle X26-22-10-01-1 000-26-310-761 B2622002 DIS APU Fire Extinguisher Cartridges X26-22-10-01-2 000-26-310-761 DIS APU Fire Extinguisher Cartridges X26-22-13-01 000-26-310-120 DVI APU Fire Extinguishing System Lines X

See task C26-20-131-03




A1CRJ A2

CRJ A3

CRJ A4

CRJ A5

CRJ A6

CRJ A7

CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


26-23-00-05 LC2 HYDRO CK Portable Fire Extinguisher Bottles X26-23-01-01 000-26-280-701 B0520001 GVI Lavatory Fire Extinguisher X26-23-01-03 LC2 Weight Check Portable FireEx Bottles X26-23-01-07 000-26-270-750 B2623002 Weight Check Lav Auto Fire Extinguisher X26-25-00-02 000-26-900-121 DVI Cargo Compt Fire EXT System Lines X26-25-00-04 000-26-220-103 OPC cargo compt fire extinguishing system X26-25-00-07 000-26-900-152 FNC Cargo Fire Extinguishing System X26-25-01-01 000-26-310-752 B2625001 HYDRO CK LH Cargo Fire Extinguisher Bottle X26-25-01-01 000-26-310-753 B2625002 HYDRO CK RH Cargo Fire Extinguisher Bottle X26-25-01-04 000-26-310-003 VCK Cargo Fire EXT Bottles Pressure X X X26-25-01-07 000-26-310-762 DIS Cargo Fire Bottle Squibs X27-10-12-01 000-27-220-001 OPC Aileron Trim System X X X X X X X X X X27-11-00-03 000-27-900-120 DVI Aileron Mechanical Control-Path X27-11-00-05 000-27-900-100 DVI Aileron/Autopilot Mechanical-Control-Path X27-11-00-07 000-27-900-717 B0520002 Tension Check of Aileron Control Cables X27-11-00-09 000-27-900-015 071502-A FNC (Backlash) Aileron Control System X27-11-00-11 000-27-900-004 OPC Aileron Control System X X X X X X X X X X27-11-01a TBD B2711001 DIS Aileron Flutter Damper Shear Pin (Solid) X27-11-01b TBD B2711002 DIS Aileron Flutter Damper Shear Pin X27-11-05 Task Deleted SEP 14/07 per TR 2B-212627-11-06 Task Deleted SEP 14/07 per TR 2B-212627-11-15-01 000-27-900-720 FNC Aileron Breakout Bungee, Breakout Switch X

27-13-01-01 000-27-900-001 OPC Aileron Disconnect System X X X X X X X X X X27-15-01-01 000-27-590-100 DVI LH Aileron Assembly X27-15-01-01 000-27-690-100 DVI RH Aileron Assembly X27-15-05-0127-15-05-03 000-27-590-720 FNC LH Aileron Flutter Damper X27-15-05-03 000-27-690-720 FNC RH Aileron Flutter Damper X27-15-05-0527-20-00-0327-20-00-05 000-27-900-121 DVI Rudder System Mechanical Control Path X27-20-00-07 000-27-900-718 B0520002 Tension Check of Rudder Control Cables X27-20-00-10 000-27-220-002 OPC Rudder Trim System X X X X X X X X X X27-20-00-13 000-27-900-006 OPC Rudder Control System X X X X X X X X X X27-21-06 Task Deleted SEP 14/07 per TR 2B-212627-24-05-01 000-27-320-101 DVI Rudder Assembly X27-31-00-0327-31-00-05 000-27-900-005 OPC Elevator Control System X X X X X X X X X X27-31-01a TBD B2731001 DIS Elevator Flutter Damper Shear Pin X27-31-01b TBD B2731002 DIS Elevator Flutter Damper Shear Pin X27-31-01c TBD B2731002 DIS Elevator Flutter Damper Shear Pin X27-31-01d TBD B2731002 DIS Elevator Flutter Damper Shear Pin X27-31-01e TBD B2731002 DIS Elevator Flutter Damper Shear Pin X27-31-01f TBD B2731002 DIS Elevator Flutter Damper Shear Pin X27-31-02 Task Deleted SEP 14/07 per TR 2B-212627-31-35-01 000-27-900-131 DVI Elevator System Mechanical Control Path X27-31-35-03 000-27-900-719 B0520002 Tension Check of Elevator Control Cables X27-32-01-01 000-27-900-118 FNC Pitch Disconnect System X27-34-05-0127-34-05-0327-34-05-05 000-27-330-720 FNC LH Elevator Flutter Dampers X27-34-05-05 000-27-340-720 FNC RH Elevator Flutter Dampers X27-35-01-01 LC2 DVI of the AOA vanes for freedom of movement X

27-35-01-07 000-27-220-120 OPC Stall Protection Computer X

See task C27-10-105-07

See task C27-10-105-07See task C27-10-105-05

See task C27-10-105-05





A1CRJ A2

CRJ A3

CRJ A4

CRJ A5

CRJ A6

CRJ A7

CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


27-40-01-05 000-27-320-121 Backlash Check Horiz Stab Trim Actuator X27-40-01-07 000-27-320-122 DVI Horiz Stab Trim Actuator Desiccant X27-40-01-09 000-27-220-102 FNC Horiz stab-Trim System X27-40-01-11 000-27-140-100 FNC Horiz Stab Trim-Control Unit X27-40-01-14 000-12-320-701 LUB Horiz Stab Trim Actuator Screw Jack X27-40-01-17 000-12-320-121 LUB Horiz stab Hinge Bushings X27-40-101 000-27-320-600 SDI HSTA Screw Shaft/Primary Gimbal Assembly X

27-40-102 000-27-320-601 SDI HSTA Pins X27-42-01 AD2002-16-02 Part Master

FileDIS Horiz Stab Trim Actuating Sys Act X

27-50-01-01 000-27-160-002 DVI Flap Power-Drive-Unit X X27-50-01-01 000-27-580-003 DVI LH Inboard Flap X X27-50-01-01 000-27-590-003 DVI LH Outboard Flap X X27-50-01-01 000-27-680-003 DVI RH Inboard Flap X X27-50-01-01 000-27-690-003 DVI RH Outboard Flap X X27-50-01-03 000-12-580-700 B0520002 LUB LH Inboard Flap X27-50-01-03 000-12-590-703 B0520002 LUB LH Outboard Flap X27-50-01-03 000-12-680-700 B0520002 LUB RH Inboard Flap X27-50-01-03 000-12-690-703 B0520002 LUB RH Outboard Flap X27-50-01-04 000-12-580-001 LUB LH Inboard Flap Actuators X X X X X X X X X X27-50-01-04 000-12-590-001 LUB LH Outboard Flap Actuators X X X X X X X X X X27-50-01-04 000-12-680-001 LUB RH Inboard Flap Actuators X X X X X X X X X X27-50-01-04 000-12-690-001 LUB RH Outboard Flap Actuators X X X X X X X X X X27-50-01-05 000-27-900-110 FNC Flap System X27-50-01-0727-50-01-0827-50-01-09 000-27-160-001 DVI Flap Flexible Drive-Shaft 1 Casing X X X X27-50-01-09 000-27-580-001 DVI LH Flap Flex Drive-Shaft 2 Casing X X X X27-50-01-09 000-27-590-001 DVI LH Flap Flex Drive-Shaft 3 to 5 Casing X X X X27-50-01-09 000-27-680-001 DVI RH Flap Flex Drive-Shaft 2 Casing X X X X27-50-01-09 000-27-690-001 DVI RH Flap Flex Drive-Shaft 3 to 5 Casing X X X X27-50-01-10 000-27-160-103 DVI Flap Flexible Drive-Shaft 1 Core X27-50-01-10 000-27-580-103 DVI LH-Wing Flap Flex Drive-Shaft 2 Core X27-50-01-10 000-27-590-104 DVI LH Flap Flex Drive-Shaft 3 to 5 Core X27-50-01-10 000-27-680-103 DVI RH Flap Flex Drive-Shaft 2 Core X27-50-01-10 000-27-690-104 DVI RH-Wing Flap Flexible Drive-Shaft 3-5 X27-51-00-01 000-27-900-007 OPC Skew Detection System (IBIT) X X X X X X X X X X27-51-10 TBD Part Master

FileDIS Flap Cntl Sys Sensor Unit X

27-53-01a TBD DIS Flap Actuating Mech Sys Act - INBD Flap

27-53-01b TBD Part Master File

DIS Flap Actuating Mech Sys Act - INBD Flap X

27-53-01c TBD Part Master File

DIS Flap Actuating Mech Sys Act - INBD Flap X

27-53-05a TBD DIS Flap Actuating Mech Sys Act - OUTBD Flap

27-53-05b TBD DIS Flap Actuating Mech Sys Act - OUTBD Flap

27-53-05c TBD Part Master File

DIS Flap Actuating Mech Sys Act - OUTBD Flap X

27-53-05d TBD Part Master File


27-53-05e TBD DIS Flap Actuating Mech Sys Act - OUTBD Flap

Part effective to this task is not in CHQ system or on CHQ aircraft.








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27-53-05f TBD DIS Flap Actuating Mech Sys Act - OUTBD Flap

27-53-05g TBD Part Master File


27-53-05h TBD Part Master File


27-53-10 TBD DIS Flap Actuating Mech Sys Shaft Assembly X27-54-15a TBD B2754001 DIS Inboard Flap Vane Actuator Assembly X27-54-15b TBD DIS Inboard Flap Vane Actuator Assembly X27-54-15c TBD DIS Inboard Flap Vane Actuator Assembly X27-60-01-01 000-27-900-111 FNC Spoiler Control System X27-60-01-03 000-27-900-133 DVI LH Spoileron, Flt/Gnd Spoilers X27-60-01-03 000-27-900-134 DVI RH Spoileron, Flt/Gnd Spoilers X27-60-01-05 000-27-160-101 DVI Inbd/Outbd Gnd Spoil Cntl-Valve Manifold X27-60-01-05 000-27-900-135 DVI LH Spoiler PCUs, Gnd Spoiler Actuators X27-60-01-05 000-27-900-136 DVI RH Spoiler PCUs, Gnd Spoiler Actuators X27-60-01-07 000-27-900-003 OPC Manual Roll Priority System X X X X X X X X X X27-60-01-09 000-27-900-149 OPC Spoiler/Fht Spoiler Autostow Circuit X27-60-01-11 000-27-140-102 OPC Spoiler Electronic Control Unit X27-60-01-11 000-27-900-112 OPC Spoiler System X27-60-01-15 000-27-900-716 FNC Spoiler Ground Lift Dump (GLD) X28-11-00-01 LC1 GVI fuel access panel, fuel/water drain valve X28-11-00-02 000-28-900-752 VCK Wing Tank Fasteners X28-11-00-05 LC1 OPC water drain valves to collect water X28-11-00-07 000-28-900-751 VCK Fuel Filler-Cap "O" Ring X28-11-00-601 000-28-900-140 DVI Critical Bonding Jumpers X28-11-00-602 000-28-900-141 FNC Critical Bonding Jumpers X28-11-00-603 000-28-900-142 DVI Sealant on In-Tank LRUs X28-11-00-604 000-24-900-140 DVI fuel tank wiring harness front and rear spar

condition and security X

28-11-00-604 000-24-900-141 DVI fuel tank wiring harness front and rear spar condition and security X

28-11-00-604 000-24-900-142 DVI fuel tank wiring harness front and rear spar condition and security X

28-12-00-01 LC1 OPC main/center fuel tank Press relief valve X28-12-00-03 000-28-900-753 Press Lk Test Fuel Tank Vent/Line Shrouds X28-21-00-03 000-28-900-700 B0520001 OPC Eng Fuel Shutoff-Valves X28-21-00-05 000-28-900-750 FNC Collector Tank Check Valve X28-24-00-03 000-28-900-701 B0520001 OPC APU Fuel-Feed Shutoff Valve X28-24-00-05 000-28-160-700 RST APU Fuel Pump Brushes X X X X28-24-01 TBD B2824001 DIS APU Fuel Feed Sys Cartridge X29-00-00-01 000-29-900-100 Hydraulic Fluid Analysis X29-11-00-03 000-29-900-101 INT Leak Check Hydraulic System X29-11-03 TBD B2911001 DIS Hyd Sys No.1 & No.2 Pump (ACMP) X29-11-05-01 000-29-310-001 VCK HYD SYS 1&2 Filter delta-p Indicators X X X X X X X X X X29-11-09-01 000-29-310-700 B0520002 DIS HYD SYS 1 Press-Manifold Filter-Element X29-11-09-01 000-29-310-701 B0520002 DIS HYD SYS 2 Press-Manifold Filter-Element X29-11-11-01 LC2 VCK Hyd Sys 1&2 accumulators for nitrogen X29-11-30-01 000-29-310-706 B2911002 DIS HYD SYS 1 and 2 RES Mounted Check-

Valves X

29-11-30-03 000-29-310-707 B2911003 DIS HYD SYS 1 and 2 Return-Line Check-Valves X

29-11-36-01 000-29-900-102 OPC HYD SYS 1 and 2 Firewall SOV's X29-11-38-01 000-29-310-001 VCK HYD SYS 1&2 Filter delta-p Indicators X X X X X X X X X X29-11-40-01 000-29-310-702 B0520002 DIS HYD SYS 1 Case-Drain Filter-Element X29-11-40-01 000-29-310-703 B0520002 DIS HYD SYS 2 Case-Drain Filter-Element X





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29-11-42-01 000-29-310-106 DVI HYD SYS 1 and 2 Heat Exchanger Cores X29-11-44-01 000-29-310-001 VCK HYD SYS 1&2 Filter delta-p Indicators X X X X X X X X X X29-11-46-01 000-29-310-704 DIS HYD SYS 1 Return Manifold Filter-Element X

29-11-46-01 000-29-310-705 DIS HYD SYS 2 Return Manifold Filter-Element X

29-12-00-03 000-29-900-101 INT Leak Check Hydraulic System X29-12-05-01 000-29-160-001 VCK HYD SYS 3 Filter Diff Press Indicators X X X X X X X X X X29-12-09-01 000-29-160-700 B0520002 DIS HYD SYS 3 Press-Manifold Filter-Element X29-12-11-01 LC2 VCK Hyd Sys 3 accumulator for nitrogen X29-12-30-01 000-29-160-703 B2912001 DIS HYD SYS 3 Return Manifold Check-Valve X29-12-30-03 000-29-160-704 B2912001 DIS HYD SYS 3 Return Manifold Check Valve X29-12-34-01 000-29-160-001 VCK HYD SYS 3 Filter Diff Press Indicators X X X X X X X X X X29-12-36-01 000-29-160-701 B0520002 DIS HYD SYS 3A, 3B Case-Drain Filter-Elements X

29-12-36-03 000-29-160-702 DIS HYD SYS 3 Return Manifold Filter-Element X

29-12-38-01 000-29-160-001 VCK HYD SYS 3 Filter Diff press Indicators X X X X X X X X X X29-33-01-601 000-29-220-100 FNC HYD SYS 1, 2, and 3 RES Temp Xducers X

29-33-01-602 000-29-900-160 B2933001 DIS HYD SYS 1, 2, and 3 Reservoir Xducers X30-12-00-01 000-30-220-100 OPC Wing Anti-Ice Stby Mode X30-12-12-0130-12-16-01 000-30-900-101 OPC Wing Anti-Ice Stby Thermal Switches X30-12-23-0131-31-03-01 000-31-360-720 FNC FDR Underwater Locator Device X31-31-03-03 000-31-360-760 RST FDR Underwater Locator Device X X X X X X X X X X31-31-03-09 000-31-900-130B FNC FDR Dedicated Sensors X31-41-00-01 000-31-220-100 OPC EICAS Aural-Warning System X31-41-00-03 000-31-220-101 OPC EICAS Reversionary Mode X31-41-04-0131-41-04-0331-41-04-04 000-31-220-700 B0520002 OPC Data Concentrator Units X31-41-04-05 000-31-140-100 OPC Data Concentrator-Unit Fans X32-00-00-01 000-32-710-001 GVI NLG Components and Doors X X X X X X X X X X32-00-00-01 000-32-730-001 GVI LH MLG Components and Door X X X X X X X X X X32-00-00-01 000-32-740-001 GVI RH MLG Components and Door X X X X X X X X X X32-00-00-03 000-12-710-001 LUB Nose Landing Gear X X X X X X X X X X32-00-00-03 000-12-730-001 LUB LH Main Landing Gear X X X X X X X X X X32-00-00-03 000-12-740-001 LUB RH Main Landing Gear X X X X X X X X X X32-00-00-04 LC2 LUB trailing arm Up/Lwr shock strut joint MLG X32-00-00-05-1 000-32-730-760 RST LH Main Landing Gear Assembly X32-00-00-05-1 000-32-740-760 RST RH Main Landing Gear Assembly X32-00-00-05-10 000-32-710-764 RST NLG Uplock Assembly X32-00-00-05-10 000-32-730-765 RST LH Main Landing Gear Uplock Assembly X32-00-00-05-10 000-32-740-765 RST RH Main Landing Gear Uplock Assembly X32-00-00-05-2 000-32-730-762 RST LH Main Landing Gear Trailing Arm X32-00-00-05-2 000-32-740-762 RST RH Main Landing Gear Trailing Arm X32-00-00-05-3 000-32-730-764 RST LH Main Landing Gear Sidestay Actuator X32-00-00-05-3 000-32-740-764 RST RH Main Landing Gear Sidestay Actuator X32-00-00-05-4 000-32-710-762 RST NLG Axle Assembly X32-00-00-05-4 000-32-730-763 RST LH Main Landing Gear Axle Assembly X32-00-00-05-4 000-32-740-763 RST RH Main Landing Gear Axle Assembly X32-00-00-05-5 000-32-730-761 RST LH Main Landing Gear Shock Strut X32-00-00-05-5 000-32-740-761 RST RH Main Landing Gear Shock Strut X32-00-00-05-6 000-32-710-761 RST Drag Brace Assembly X

See task C30-10-141-01

See task C30-10-141-01





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32-00-00-05-7 000-32-710-760 RST NLG Assembly and Shock Strut X32-00-00-05-8 000-32-710-760 RST NLG Assembly and Shock Strut X32-00-00-05-9 000-32-710-763 RST NLG Extension/Retraction Actuator X32-00-00-07 Task Deleted R. 11 Part 1 MRM.32-00-00-09 LC2 DVI MLG/NLG shock strut for leak, cond, & sec X

32-00-00-11 000-32-710-002 FNC NLG Shock Strut Extension X X X X X X X X X X32-00-00-11 000-32-730-002 FNC LH MLG Shock Strut Extension X X X X X X X X X X32-00-00-11 000-32-740-002 FNC RH MLG Shock Strut Extension X X X X X X X X X X32-00-00-13 000-32-043-026 LUB MLG/NLG Axle thread & Axle Nuts X32-00-00-13 000-32-041-001A LUB MLG/NLG Axle thread & Axle Nuts X32-00-00-13 000-32-041-001B LUB MLG/NLG Axle thread & Axle Nuts X32-00-00-15 000-32-043-026 DVI MLG & Nose Axles for Corrosion & Damage X

32-00-00-15 000-32-041-001A DVI MLG & Nose Axles for Corrosion & Damage X

32-00-00-15 000-32-041-001B DVI MLG & Nose Axles for Corrosion & Damage X

32-00-00-17-1 TBD DIS the Main Landing Gear (MLG) Main Ftgs X32-00-00-17-2 TBD DIS Main Landing Gear (MLG) Trailing Arm X32-00-00-17-3 TBD DIS MLG Down Lock/Sidestay Actuator X32-00-00-17-4 TBD DIS MLG and Nose Landing Gear (NLG) Axle X32-00-00-17-5 TBD DIS Main Landing Gear (MLG) Shock Strut X32-00-00-17-6 TBD DIS Nose Downlock/Drag Brace X32-00-00-17-7 TBD DIS Nose Landing Gear (NLG) Shock Strut X32-00-00-17-8 TBD DIS Nose Landing Gear (NLG) Main Ftgs X32-00-00-19 000-32-710-100 DVI NLG Components X32-00-00-19 000-32-730-100 DVI LH MLG Components X32-00-00-19 000-32-740-100 DVI RH MLG Components X32-00-00-20 000-32-710-700 B0520002 DVI NLG Doors X32-00-00-20 000-32-730-700 B0520002 DVI LH Main-Landing Gear (MLG) Door X32-00-00-20 000-32-740-700 B0520002 DVI RH Main-Landing Gear (MLG) Door X32-00-00-21 000-12-710-002 SVC Nose Landing Gear Shock Strut X X32-00-00-21 000-12-730-002 SVC LH Main Landing Gear Shock Strut X X32-00-00-21 000-12-740-002 SVC RH Main Landing Gear Shock Strut X X32-11-102 TBD DIS Trailing Arm X32-11-104 TBD DIS MLG Assembly Side Stay Ftgs Shaft X32-11-105 TBD DIS MLG Assembly Uplock Assembly X32-11-106a TBD DIS MLG Assembly Cylinder-Piston X32-11-106b TBD DIS MLG Assembly Cylinder-Piston X32-11-107 TBD DIS MLG Assembly Shock Strut Pin X32-11-108a TBD DIS MLG Assembly Trailing Arm X32-11-108b TBD DIS MLG Assembly Trailing Arm X32-11-108c TBD DIS MLG Assembly Trailing Arm X32-11-108d TBD DIS MLG Assembly Trailing Arm X32-11-110a TBD DIS MLG Assembly Main Ftgs X32-11-110b TBD DIS MLG Assembly Main Ftgs X32-11-110c TBD DIS MLG Assembly Main Ftgs X32-11-110d TBD DIS MLG Assembly Main Ftgs X32-11-110e TBD DIS MLG Assembly Main Ftgs X32-11-110f TBD DIS MLG Assembly Main Ftgs X32-11-110g TBD DIS MLG Assembly Main Ftgs X32-11-110h TBD DIS MLG Assembly Main Ftgs X32-11-111 TBD DIS MLG Assembly Axle X32-11-112 TBD DIS MLG Assembly Side Stay Actuator Cylinder X




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32-11-113 TBD DIS MLG Assembly Side Stay Actuator Piston X

32-11-114 TBD DIS MLG Assembly Side Stay Actuator Rod End X

32-11-116 TBD DIS MLG Assembly Pivot Pin X32-11-117 TBD DIS MLG Assembly Side Stay Actuator Pin X32-11-118 TBD DIS MLG Assembly Pintle Pin X32-21-101a TBD DIS Nose Landing Gear (NLG) Assembly X32-21-101b TBD DIS Nose Landing Gear (NLG) Assembly X32-21-101c TBD DIS Nose Landing Gear (NLG) Assembly X32-21-101d TBD DIS Nose Landing Gear (NLG) Assembly X32-21-101e TBD DIS Nose Landing Gear (NLG) Assembly X32-21-101f TBD DIS Nose Landing Gear (NLG) Assembly X32-21-101g TBD DIS Nose Landing Gear (NLG) Assembly X32-21-101h TBD DIS Nose Landing Gear (NLG) Assembly X32-21-101k TBD DIS Nose Landing Gear (NLG) Assembly X32-21-102a TBD DIS NLG Assembly Uplock X32-21-102b TBD DIS NLG Uplock Assembly X32-21-103 TBD DIS Nose Landing Gear (NLG) Drag Brace X32-21-104a TBD DIS NLG Uplock Assembly X32-21-104b TBD DIS NLG Uplock Assembly X32-34-00-01 000-32-900-702 B0520002 DVI NLG and MLG Manual-Release System X32-34-00-03 000-32-900-703 B0520002 FNC NLG and MLG Manual-Release System X32-40-00-01 LC1 VCK MLG/NLG tire assemblies for damage/wear X

32-40-00-03 LC1 FNC MLG/NLG wheel assemblies for inflation X32-40-00-05 LC1 VCK MLG/NLG tires for tread depth X32-43-06-01 LC2 FNC brake accumulator Press & service X32-43-06-03 000-32-160-100 FNC Brake System Volumetric Fuses X32-43-06-05 000-12-120-001 LUB Brake Control Valve X X32-43-16-01 LC2 GVI brake Sys Hyd lines/components X32-43-21-01 000-32-900-103 DVI Park/Main Brake-Control Mechanical Path X32-43-26-01 LC1 DVI of the Brake wear indicators X32-44-00-01 000-32-900-001 FNC Antiskid Control Unit X X X X X X X X X X32-45-00-01 000-12-220-001 LUB Parking Brake Handle Slider and Track X X X X X32-50-01-05 000-32-710-100 DVI NLG Components X32-50-01-09 000-12-710-001 LUB Nose Landing Gear X X X X X X X X X X32-60-01-01 000-32-140-001 FNC Proximity Sensor Electronics Unit X X X X X X X X X X32-700-01 000-32-710-320 GVI EXT NLG Assembly X32-700-02 000-32-730-300 GVI EXT LH Main Landing Gear Assembly X32-700-03 000-32-740-300 GVI EXT RH Main Landing Gear Assembly X33-42-00-01 000-33-570-101 GVI LH Wing-Tip Position-Light Lens X33-42-00-01 000-33-670-101 GVI RH Wing-Tip Position-Light Lens X33-50-00-01 000-33-900-001 OPC Emergency Lights X X X X X X X X X X33-50-00-03 Task Deleted R. 11 Part 1 MRM.33-50-00-05 000-33-900-722 GVI Emergency floor path lighting33-51-04-01 000-33-900-701 E3350047 RST Emergency Lights Battery-Packs X33-51-04-03 000-33-900-100 OPC Emergency Lights-Battery Packs X33-51-04-05 000-33-900-720 FNC Door Exit-Sign Beta Lights X34-11-00-01 000-34-900-001 DVI Main and Standby Pitot-Static Drains X X X X X X X X X X34-11-00-05 000-34-900-121 GVI main pitot−static and standby pitot

probes X X X X X X X X X X

34-11-00-07 000-34-900-122 FNC Main and Standby Pitot Static System X34-11-01 TBD Part Master

FileDIS Pitot-Static & Temp Sensing Sys Probe X

34-12-01-01 000-34-220-720 B3412001 RST Standby Airspeed/Altimeter Indicator X

Not istalled on CHQ fleet at this time.




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34-12-01-03 000-34-220-724 FNC Integrated Stby Instrument System (ISIS) X34-13-01-01 000-34-900-720 FNC Air Data Computer Overspeed Warning X34-13-01-03 000-34-220-120 FNC Alt Scale Error and MACH/Speed Indication X

34-22-01-01 000-34-220-730 B3422001 FNC Standby Compass (Swing) X34-25-11-01 000-34-220-101 OPC EFIS Display Reversionary Switches X34-32-07-01 000-34-130-100 DVI Drive Electronic Unit Fan Filter X34-45-00-01 000-34-220-102 OPC Inertial Reference System (ATT Mode) X35-11-03-01 000-35-140-730 B3511001 HYDRO CK Crew Oxygen Cylinder X35-11-03-0335-11-03-05 000-35-140-760 B3511002 DIS Crew Oxygen Cylinder X35-11-05-01 000-35-900-100 OPC Crew Oxygen System X35-11-05-03 000-35-220-700 DVI Crew Oxygen Masks X X35-23-07-01 000-35-900-720 OPC Pax Oxygen System X35-23-07-03 000-35-900-720 OPC Pax Oxygen System X35-23-07-05 000-35-900-705 DVI Pax Oxygen Masks X35-23-13-03 000-35-900-760 DIS Oxygen Generator X35-23-13-05 000-35-900-720 OPC Pax Oxygen System X35-31-05-01 LC2 HYDRO CK Portable Oxygen Bottles X35-31-05-03 000-35-900-700 B0520001 OPC Portable Oxygen Bottles X35-31-05-05 000-25-900-700 B0520001 Inspect Emergency Equipment X35-31-07-03 LC2 DIS PBE Unit X36-11-10-01 000-36-310-101 DVI APU Air Supply Check-Valve X36-21-07-01 000-36-900-700 OPC LH Wing Leading Edge Thermal Switches X

36-21-07-01 000-36-900-701 OPC RH Wing Leading Edge Thermal Switches X

38-11-01-01 000-38-140-700 B0520001 RST Galley Water-Tank Filter X38-11-01-07 000-12-900-702 B3811001 Sanitize Galley Potable Water System X38-11-01-07 000-12-900-703 B3811001 Sanitize Lavatory Potable Water System X38-21-01-01 000-38-280-700 B0520001 RST Lavatory Water-Tank Filter X38-30-01-01 000-38-270-720 DVI Toilet Waste Tank and Drain Valve X38-30-01-03 000-38-270-720 DVI Toilet Waste Tank and Drain Valve X49-11-00-01 000-49-310-100 DVI APU Enclosure and Mounting Skid Assy X49-12-00-01 000-49-310-100 DVI APU Enclosure and Mounting Skid Assembly X

49-14-00-01 000-49-310-005 DVI APU Air Intake Duct Ext X X X49-14-00-03 000-49-310-101 DVI APU Air-Intake Assembly Desiccant X49-14-19-01 000-49-310-712 DVI APU Air Intake Door Assembly X49-15-00-01 000-49-310-132 DVI APU Drain System Tubes and Hoses X49-20-00-01 000-49-310-706 B4920001 RST Auxiliary Power Unit (HSI) X49-20-00-03 000-49-310-002 GVI APU X X X49-20-00-17 000-49-310-002 GVI APU X X X49-20-01 CRJAPURR B4920002 Discard APU Compressor Rotor X49-20-02 CRJAPURR B4920003 Discard APU Turbine Rotor X49-24-00-03 000-49-310-701 B2424001 INSP APU Fuel and Oil System X49-24-00-05 000-49-310-701 B2424001 INSP APU Fuel and Oil System X49-24-00-07 000-49-310-002 GVI APU X X X49-24-00-11 000-49-310-731 DVI APU Gearbox Vent Line X X X X49-26-00-01 000-49-310-004 GVI APU Ducts X X X49-31-00-01 000-49-310-701 B2424001 INSP APU Fuel and Oil System X49-31-05-01 000-49-310-701 B2424001 INSP APU Fuel and Oil System X49-31-05-03 000-49-310-703 DIS APU Fuel Filter Element X X X X X X X X X X49-42-10-01 000-49-310-702 B4942001 DVI APU Igniter Plugs and Leads X49-43-00-01 000-49-900-100 OPC APU-Emergency Remote-Shutoff Switches X

See task C35-10-128-01




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49-44-00-01 000-49-310-709 B4944001 DVI APU Starter Brush X49-60-00-01 000-49-310-707 VCK APU Wiring Harness and Connectors X X49-81-00-01 000-49-310-711 DVI APU Exhaust Installation X X49-91-00-05 000-49-310-003 GVI APU Oil System EXT Plumbing X X X49-91-07-01 000-49-310-710 B4991001 RST APU Oil Cooler X49-91-10-01 000-49-310-701 B2424001 INSP APU Fuel and Oil System X49-91-10-03 000-49-310-704 DIS APU Oil Filter Element X X X X X X X X X X52-00-00-01-1 000-12-810-001 LUB Main-Avionics Compartment Door X X X X X52-00-00-01-2 000-12-840-001 LUB Service Door X X X X X52-00-00-01-3 000-12-830-002 LUB Cargo Compartment Door X X X X X52-00-00-01-4 000-12-310-001 LUB Aft Equipment Compartment Door X X X X X52-00-00-02 000-12-830-003 LUB Phase III Pax Door Latch Pins X X X X X X X X X X52-00-00-03-1 000-52-830-100 DVI Crew Escape Hatch X52-00-00-03-2 000-52-830-102 DVI LH Overwing Emergency Exit X52-00-00-03-2 000-52-840-101 DVI RH Overwing Emergency Exit X52-00-00-03-3 000-52-900-100 DVI Maintenance SVC Doors X52-00-00-04 000-12-830-001 LUB Phase III Pax Door X X X X X52-00-00-05-1 000-52-830-001 FNC Phase III Pax Door X X52-00-00-05-2 000-52-840-001 FNC Service Door X X52-00-00-06-1 000-52-830-107 DVI INT Components Phase III Pax Door X52-00-00-06-2 000-52-840-103 DVI Service Door X52-00-00-07-1 000-52-810-001 DVI Main-Avionics Compartment Door X X52-00-00-07-2 000-52-210-001 DVI Fwd-Equipment Compartment Doors X X52-00-00-07-3 000-52-210-001 DVI Fwd-Equipment Compartment Doors X X52-00-00-07-4 000-52-310-001 DVI Aft-Equipment Compartment Door X X52-00-00-08 000-52-830-002 DVI Cargo Compartment Door X X X52-00-00-09-1 000-12-830-100 LUB Crew Escape Hatch X52-00-00-09-2 000-12-830-101 LUB LH Overwing-Emergency Exit X52-00-00-09-2 000-12-840-100 LUB RH Overwing-Emergency Exit X52-00-00-09-3 000-12-900-100 LUB Maintenance Service Doors X52-00-00-11-1 000-52-830-103 FNC Crew Escape Hatch X52-00-00-11-2 000-52-830-104 FNC LH Overwing Emergency Exit X52-00-00-11-3 000-52-840-102 FNC RH Overwing Emergency-Exit X52-00-00-17-1 000-52-830-003 DVI EXT Components Phase III Pax Door X X X X X52-00-00-17-2 000-52-840-002 DVI EXT Components Service Door X X X X X52-00-00-18 000-12-830-004 LUB Phase III Pax Door Outer Handle X X X X X X X X X X52-00-00-19 000-12-830-005 LUB Phase III Pax Door Outer Handle X X52-00-00-20 000-52-830-702 B0520001 DVI Crew Escape Hatch Mechanism (INT and

EXT) X

52-11-00-01 000-52-830-106 DVI Phase IV Pax Door X52-11-00-02 000-52-830-106 DVI Phase IV Pax Door X52-11-00-03 000-12-830-007 LUB Phase IV Pax Door Hinge X X X X X52-11-00-04 000-52-830-105 FNC Phase IV Pax Door X52-11-00-05 000-12-830-006 LUB Phase IV Pax Door Latch Pins/Cam X X X X X X X X X X52-11-00-06 000-52-830-106 DVI Phase IV Pax Door X52-11-02 TBD B5211001 DIS Pax Door Torsion Spring - Lock Mechanism X

52-11-02-01 000-52-830-500 DVI Pax Door Pin Ftgs and Attachments X52-11-03 TBD B5211002 DIS Pax Door Spring - Outer Handle X52-11-03-01 000-52-830-507 DVI Pax Door INT Structure X52-11-04 TBD B5211003 DIS Pax Door Bushing - Upper Latch Ftgs X52-11-08 TBD DIS Pax Door Motor - Pax Door X52-11-101a 000-52-830-602 SDI Pax Door INT and EXT Structure X52-11-101b TBD DVI Pax Door INT and EXT Structure X52-11-102 000-52-830-600 DVI Pax Door Bracket, Hinge & Support Struct X52-11-104a 000-52-830-605 SDI Phase IV Pax Door INT and EXT Structure X




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CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


52-11-104a TBD DVI Phase IV Pax Door INT and EXT Structure X52-11-105 000-52-830-606 DVI Phase IV Pax Door Bracket, Hinge/Support X

52-11-131 000-52-830-612 B5211004 Detailed Inspection of the Pass door − piano hinge half on door side X

52-21-02-01 000-52-830-501 DVI LH Emerg-Exit Latch Ftgs and Door Stops X52-21-02-01 000-52-840-500 DVI RH Emergency Exit Latch Ftgs/Stops X52-21-03-01 000-52-830-502 DVI LH Emerg-Exit INT Support Structure X52-21-03-01 000-52-840-501 DVI RH Emerg-Exit INT Support Structure X52-21-102 000-52-830-601 DVI LH Overwing Emergency Exit Door X X X X X52-21-102 000-52-840-600 DVI RH Overwing Emergency Exit Door X X X X X52-21-104 000-52-830-607 DVI LH Overwing Emergency Exit Door X52-21-104 000-52-840-602 DVI RH Overwing Emergency Exit Door X52-21-105 000-52-830-609 DVI LH Overwing Emergency Exit Door Casting X X X X X

52-21-105 000-52-840-603 DVI RH Overwing Emergency Exit Door Casting X X X X X

52-22-02-01 000-52-830-503 DVI Crew Escape Hatch Pin Ftgs/Stops X52-22-03-01 000-52-830-505 DVI Crew Escape Hatch Stop Support Structure X

52-22-102 000-52-830-603 DVI Crew Escape Hatch Ftgs, Bracket/Structure X

52-22-103 000-52-830-608 DVI Crew Escape Hatch Ftgs, Bracket & Support X

52-31-02-01 000-52-830-504 DVI Cargo Door Stop Ftgs X52-31-03-01 000-52-830-506 DVI Cargo Door INT Structure X52-31-102 000-52-830-604 DVI Cargo Door Structure X52-41-02-01 000-52-840-503 DVI Service Door Stops and Ftgs X52-41-03-01 000-52-840-502 DVI Service Door INT Support Structure X52-41-102 000-52-840-601 DVI Service Door Ftgs/Back-up Structure X52-42-02-01 000-52-810-501 DVI Main Avionics Compartment Door-Stops X52-42-03-01 000-52-810-500 DVI Main Avionics Compt Door Stop Structure X52-42-103 000-52-810-600 DVI Avionics Compt Door Ftgs/Backup Structure X

52-700-01 000-52-710-330 GVI EXT Nose Landing Gear Doors X52-700-02 000-52-710-330 GVI EXT Nose Landing Gear Doors X52-700-03 000-52-710-330 GVI EXT Nose Landing Gear Doors X52-700-04 000-32-730-301 GVI EXT LH Main Landing Gear Door X52-700-05 000-32-740-301 GVI EXT RH Main Landing Gear Door X52-800-01 000-52-810-300 GVI EXT Main Avionics Compartment Door X52-800-02 000-52-810-320 GVI INT Main Avionics Compartment Door X52-800-03 000-52-830-320 GVI EXT Crew Escape Hatch X52-800-04 000-52-830-321 GVI INT Crew Escape Hatch X52-800-05 000-52-830-300 GVI EXT and INT Pax Door X52-800-06 000-52-830-300 GVI EXT and INT Pax Door X52-800-07 000-52-830-322 GVI EXT LH Overwing Emergency Exit X52-800-07 000-52-840-320 GVI EXT RH Overwing Emergency Exit X52-800-08 000-52-830-323 GVI INT LH Overwing Emergency Exit X52-800-08 000-52-840-321 GVI INT RH Overwing Emergency Exit X52-800-09 000-52-830-301 GVI EXT Cargo Compartment Door X52-800-10 000-52-830-302 GVI INT Cargo Compartment Door X52-800-11 000-52-840-300 GVI EXT Service Door X52-800-12 000-52-840-322 GVI INT Service Door X53-100-01 000-53-110-320 GVI EXT Radome X53-100-02 000-53-110-330 GVI INT Radome X53-100-03 000-53-120-330 GVI EXT Fuse Nose Skin X




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CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


53-100-04 000-53-120-300 GVI INT Nose Hydraulics Compartment X53-100-05 000-53-120-301 GVI INT Air Driven Generator Compartment X53-100-06 000-53-120-320 GVI INT Nose Wheel Well X53-100-07 000-53-130-320 GVI EXT LH Fwd Fuse X53-100-07 000-53-130-321 GVI EXT RH Fwd Fuse X53-100-08 000-53-130-300 GVI INT LH Fwd Avionic/Flt deck X53-100-09 000-53-130-322 GVI INT RH Fwd Avionics and Flt Deck X53-100-10 000-53-140-320 GVI EXT Fwd/Mid Fuse below WL73.50 X53-100-11 000-53-140-321 GVI INT Main Avionics Compartment X53-100-12 000-53-140-321 GVI INT Main Avionics Compartment X53-100-13 000-53-150-320 GVI EXT Mid Fuse/Fw Wing-to-Fuse Fairings X53-100-14 000-53-150-321 GVI INT Fwd ECS Compartment X53-100-15 000-53-150-321 GVI INT Fwd ECS Compartment X53-100-16 000-53-160-320 GVI EXT Overwing-to-Fuse Panels X53-100-17 000-53-160-321 GVI INT Mid Lwr Fuse Below Floor X53-100-18 000-53-160-321 GVI INT Mid Lwr Fuse Below Floor X53-100-19 000-53-160-300 GVI INT LH Main Landing Gear Wheel Well X53-100-20 000-53-160-301 GVI INT RH Main Landing Gear Wheel Well X53-100-21 000-53-160-322 GVI INT Mid Lwr Fuse X53-100-22 000-53-170-320 GVI EXT Aft and Wing to Fuse Fairings X53-100-23 000-53-170-321 GVI INT Aft ECS Compartment X53-100-26 000-53-170-321 GVI INT Aft ECS Compartment X53-11-01-01 000-53-120-502 DVI Fwd Fuse Frames X53-11-02-01 000-53-120-503 DVI Fwd Pressure Bulkhead Aft Face X53-11-03-01 000-53-900-507 DVI LH INT Skin, Stringers and Frames X53-11-03-01 000-53-900-508 DVI RH INT Skin, Stringers and Frames X53-11-05-01 000-53-220-505 DVI LH Windshield Side Post Supports X53-11-05-01 000-53-220-506 DVI RH Windshield Side Post Supports X53-11-06-01 000-53-220-502 DVI Flight Compartment INT Ceiling structure X53-11-07-01 000-53-220-507 DVI Crew Escape Hatch Stop Ftgs on Fuse X53-11-08-01 000-53-900-507 DVI LH INT Skin, Stringers and Frames X53-11-08-01 000-53-900-508 DVI RH INT Skin, Stringers and Frames X53-11-09-01 000-53-900-502 DVI Flt Compt Bulkhead and Fuse Frame X53-11-10-01 000-53-130-501 DVI Flt Compt Floor Beams and Crossmembers X

53-11-101-1 000-53-710-600 DVI NLG, Drag Strut, Trunnion Ftgs, Structure X53-11-101-2 000-53-710-600 DVI NLG, Drag Strut, Trunnion Ftgs, Structure X53-11-102 000-53-130-601 DVI NLG Wheel Well Vert Stiffener Lwr Attach X53-11-103 000-53-130-602 DVI NLG Wheel Well Upper Cap Angles X53-11-104 000-53-220-600 DVI Flt Dk Floor Attach-Fwd Pressure Bulkhead X

53-11-106 000-53-900-600 DVI Fwd Pressure Bulkhead Vert Stiffeners/Web X

53-11-108-1 000-53-130-603 DVI Frame FS235.0 Lwr Sector Web and Caps X

53-11-108-2 000-53-130-603 DVI Frame FS235.0 Lwr Sector Web and Caps X

53-11-110 000-53-830-600 DVI Flt Crew Escape Hatch Structure X53-11-11-01 000-53-220-503 DVI Flight Compartment Floor Panels X53-11-11-02 000-53-220-500 DVI Flight Compartment Floor Seat Rails X53-11-112 000-53-130-604 DVI Fuse Skin at Cockpit Floor Level X53-11-121 000-53-220-601 SDI Cockpit Side Window Aft End Post X53-11-122a 000-53-220-602 SDI Windshield Center Post and Strap X53-11-122b TBD DVI Windshield Center Post and Strap X53-11-123 000-53-220-603 SDI Windshield Side Post Up/Lwr Joints/Ftgs X53-11-124-1 000-53-130-600 DVI NLG Wheel Well Skin Cut-out X




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CRJ A8

CRJ A9

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CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


53-11-124-2 000-53-130-600 DVI NLG Wheel Well Skin Cut-out X53-11-126 000-53-130-605 DVI Flitefone V1 Antenna Cut-out X53-11-127a TBD SDI Windshield Center Post/Bulkhead Aft Post X

53-11-127b 000-53-900-611 DVI Aft Center Post at Fwd Pressure Bulkhead X

53-11-128 TBD DVI Fwd Press Bulkhead X53-11-129a TBD SDI Windshield Center Post/Bulkhead Aft Post X

53-11-129b TBD DVI Windshield Center Post/Bulkhead Aft Post X

53-11-130a TBD SDI Windshield Center Post/Bulkhead Aft Post X

53-11-130b TBD DVI Windshield Center Post/Bulkhead Aft Post X

53-11-15-01 000-53-130-500 DVI Fwd Jacking Ftgs at FS278.0 X53-11-16-01 000-53-220-504 DVI Windshield/Side Window Frames/ Posts X53-11-17-01 000-53-220-501 DVI Side Post Straps,Windshield/Side Windows X

53-11-18-01 000-53-120-500 DVI NLG Trunnion Ftgs and Diagonal Member X53-11-19-01 000-53-120-501 DVI NLG Wheel Well INT Box Structure X53-200-01 000-53-210-320 GVI EXT Fuse Skin, FS169.00 to FS202.75 X53-200-02 000-53-210-330 GVI INT LH Fwd Equipment Compartment X53-200-03 000-53-210-331 GVI INT RH Fwd Equipment Compartment X53-200-04 000-53-220-300 GVI EXT Fwd Fuse from FS202.75 - FS280.00 X53-200-05 000-53-220-301 GVI INT Flight Compartment X53-200-06 000-53-220-301 GVI INT Flight Compartment X53-200-07 000-53-900-320 GVI EXT Fwd/Mid and Center Fuse X53-200-08 000-53-230-330 GVI INT Pax Compartment Entry Area X53-200-09 000-53-230-320 GVI INT Pax Compartment Galley Area X53-200-10 000-53-900-320 GVI EXT Fwd/Mid and Center Fuse X53-200-11 000-53-240-340 GVI INT LH Pax Compartment X53-200-12 000-53-240-341 GVI INT RH Pax Compartment X53-200-30 000-53-280-320 GVI EXT Aft Fuse FS559.00+80 to FS621.00 X53-200-31 000-53-280-300 GVI INT Cargo Compartment X53-200-32 000-53-280-300 GVI INT Cargo Compartment X53-21-01-01 000-53-230-501 DVI Pax Door Upper and Lwr Sills X53-21-02-01 000-53-230-504 DVI Pax Door Cutout/Interior Backup Ftgs X53-21-02-02 000-53-900-500 DVI Pax Door Cut-out Frames X53-21-03-01 000-53-230-505 DVI Pax Door Ftgs on the Fuse X53-21-04-01 000-53-140-500 DVI Pax Door Hinge on Fuse X53-21-05-01 000-53-230-500 DVI Fuse Skin at Pax Door Cutout X53-21-06-01 000-53-840-501 DVI Fuse Skin at Service Door Cut-out X53-21-07-01 000-52-840-503 DVI Service Door Stops and Ftgs X53-21-08-01 000-53-900-509 DVI SVS Door Side Frames, Sills, Structure X53-21-08-02 000-53-840-500 DVI Exp Srv Door Side Frame, Sill/Backup Stru X

53-21-09-01 000-53-140-501 DVI Main Avionics Compt Door Ftgs X53-21-10-01 000-53-140-502 DVI INT Main Avionics Compt-Door Cut-out X53-21-101 000-53-230-600 DVI Pax Door Cut-out Upper and Lwr Sills X53-21-102 000-53-230-601 DVI Pax Door Cut-out Frames/Back-up Structure X

53-21-103 000-53-230-602 DVI Pax Door Ftgs on Fuse X53-21-108 000-53-900-601 DVI SVS Door Cut-out Frame, Sills, Structure X53-21-110 000-53-140-600 DVI Avionics Compt Door Cut-out Structure X53-21-11-01 000-53-140-505 DVI Cabin Floor Support Structure X




A1CRJ A2

CRJ A3

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CRJ A6

CRJ A7

CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


53-21-115 000-53-900-603 DVI Fuse Structure FS280.0 to FS409.0 X53-21-118 000-53-140-601 DVI INT Potable Water SVC Door Cut-out X53-21-119 000-53-900-604 DVI Fwd/Aftr Lav SVC Door Cutout/INT Struct X53-21-12-01 000-53-900-503 DVI LH Side Seat Rail Structure X53-21-12-01 000-53-900-504 DVI RH Side Seat Rail Structure X53-21-125 000-53-900-605 DVI Circumferential Fuse Splice FS280.0 X53-21-126 000-53-230-603 DVI Phase IV Pax Door Cut-out Upper/Lwr Sills X

53-21-127 000-53-230-604 DVI Phase IV Pax Door Cut-out Frame/Structure X

53-21-128 000-53-230-605 DVI Phase IV Pax Door Ftgs on Fuse X53-21-129 000-53-230-606 B5211004 Detailed Inspection of the Pass door − piano

hinge half on fuselageside

X

53-21-13-01 000-53-230-502 DVI LH INT Skin Panels, Frames and Stringers X

53-21-13-01 000-53-230-503 DVI RH INT Skin Panels, Frames and Stringers X

53-21-14-01 000-53-140-507 DVI INT Skin Panels, Frames and Stringers X53-21-17-01 000-53-140-503 DVI EXT Lwr Fuse Skin Panels X53-21-18-01 000-53-140-506 DVI Fwd Potable Water SVC Cutout X53-300-01 000-53-310-301 GVI EXT AFT Fuse, FS621.00 to FS755.00 X53-300-02 000-53-310-300 GVI INT AFT Equipment Compartment X53-300-03 000-53-350-320 GVI EXT Aft Fuse/stab Section X53-300-04 000-53-350-321 GVI INT Aft Fuse/stab Section X53-300-05 000-53-360-340 GVI EXT Tail Cone X53-300-06 000-53-360-341 GVI INT Tail Cone X53-41-01-01 000-53-150-500 DVI Floor Support Structure X53-41-02-01 000-53-900-503 DVI LH Side Seat Rail Structure X53-41-02-01 000-53-900-504 DVI RH Side Seat Rail Structure X53-41-03-01 000-53-250-501 DVI LH INT Skin Panels, Frames and Stringers X


53-41-04-01 000-53-140-507 DVI INT Skin Panels, Frames and Stringers X53-41-07-02 000-53-140-508 DVI EXT Lwr Skin Panel (Under Fairing) X53-41-08-01 000-53-150-502 DVI Fwd Keel Beams and Pressure Box X53-41-09-01 000-53-150-502 DVI Fwd Keel Beams and Pressure Box X53-41-10-01 000-53-260-502 DVI LH INT Skin Panels, Frames and Stringers X


53-41-101 000-53-900-606 DVI ADF Antenna and DME Antenna Cut-outs X53-41-103 000-53-250-600 DVI Emergency Light Cut-out at EXT Side Panel X

53-41-104 000-53-150-600 DVI Fwd Keel Beam Bayonet Ftgs X53-41-107 000-53-260-600 DVI VHF Antenna Cut-out at FS455.8 X53-41-108 000-53-260-601 DVI Skin at Str. 6 and Frames X53-41-109 000-53-260-602 B5341009 SDI Longitudinal Str. 6 Splice X53-41-110 000-53-260-603 SDI longitudinal Str 6 splice butt strap X53-41-111-1 000-53-260-604 DVI Skin Panel at Machined Frames X53-41-111-2 000-53-260-604 DVI Skin Panel at Machined Frames X53-41-112 000-53-260-605 DVI Emerg Light Cut-outs in Side Skin Panel X53-41-116 000-53-160-604 AD032003 DVI Vertical Beams on Frame X53-41-119 000-53-900-602 SDI Frame FS409.0 +128 and Frame FS559.0 X53-41-120 000-53-260-606 SDI Frame FS559.0 Splice at Str. 0 X




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CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672




53-41-124 000-53-160-605 DVI Bulkhead Webs X53-41-125 000-53-260-607 DVI LH Emerg Exit Door Cut-out Structure X53-41-125 000-53-260-608 DVI RH Emerg Exit Door Cut-out Structure X53-41-126 000-53-900-607 SDI Cabin Windows Surrounding Structure X53-41-127 000-53-260-609 SDI Circumferential Fuse Joint X53-41-128 000-53-260-610 SDI Circumferential Fuse Joint X53-41-132-1 000-53-260-611 SDI Frame FS424.0 & FS513.0 Inner/Outer Caps X

53-41-132-2 000-53-260-611 SDI Frame FS424.0 and FS513.0 Inr/Outer Caps X

53-41-133-1 000-53-160-606 DVI Frame FS424.0 Wing Attachment Lugs X53-41-133-2 000-53-160-606 DVI Frame FS424.0 Wing Attachment Lugs X53-41-134 000-53-260-612 DVI Frame FS449.85 Inner Cap X53-41-138-1 000-53-160-607 DVI Frame FS473.15 Wing Attachment Lugs X53-41-138-2 000-53-160-607 DVI Frame FS473.15 Wing Attachment Lugs X53-41-139 000-53-260-613 DVI Frames FS424.0, FS473.0 and FS513.0 X53-41-14-01 000-53-250-501 DVI LH INT Skin Panels, Frames and Stringers X


53-41-141 000-53-160-600 SDI Frame FS513.0 Under Floor BL0.0 Splice X53-41-142-1 000-53-160-608 DVI Frame FS513.0, BL0.0 Wing Attach Ftgs X53-41-142-2 000-53-160-608 DVI Frame FS513.0, BL0.0 Wing Attach Ftgs X53-41-145 000-53-160-601 SDI Overwing Floor Support Beam at FS460.0 X53-41-146 000-53-160-609 SDI Pressure Floor Skin Access Panel Cut-outs X

53-41-149 000-53-160-610 DVI Pressure Floor Skin X53-41-150 000-53-160-611 DVI Pressure Floor Support Beams X53-41-155 000-53-160-612 DVI Pressure Floor Sill FS409.0 +128-FS559.0 X

53-41-156 000-53-160-613 DVI Pressure Floor Intercostals X53-41-157 000-53-160-614 DVI Frame Attachment to Sill and Longeron X53-41-158 000-53-160-602 DVI Underfloor Longeron Assy at FS409.0 +128 X

53-41-159-1 000-53-160-615 DVI Longeron at FS424.0 X53-41-159-2 000-53-160-615 DVI Longeron at FS424.0 X X53-41-16-01 000-53-160-506 DVI Aft Face Fuse Frame FS409.0 +128 X53-41-161-1 000-53-160-616 SDI Underfloor, BL45.0, Longeron Lwr Flange X53-41-161-2 000-53-160-616 SDI Underfloor, BL45.0, Longeron Lwr Flange X53-41-162 000-53-160-617 DVI Underfloor, BL45.0, Longeron Web X53-41-163 000-53-160-618 DVI Underfloor, BL45.0, Longeron Upper Flange X

53-41-165 000-53-270-600 DVI Upper Skin Panel FS559.0 to FS559.0 +112 X

53-41-166 000-53-270-601 DVI Skin Panel FS559.0 to FS559.0 +112 X53-41-168 000-53-260-614 DVI Pressure Floor Sill Web X53-41-17-01 000-53-270-501 DVI LH INT Skin Panels, Frames and Stringers X


53-41-171 000-53-160-619 DVI Oxygen Indicator Cut-out X53-41-176 000-53-260-615 DVI GPS Antenna Cut-outs X




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CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


53-41-177 000-53-160-603 B5341001 DVI Keel Beam cutout FS409.0 +128 X53-41-179 000-53-160-621 DVI Keel Beam Cut-Out at FS409.0 +128 X53-41-180 000-53-160-627 DVI FS409+128 Bulkhead Strap Modification X53-41-18-01 000-53-170-505 DVI Aft Face Fuse Frame, FS559.0 X53-41-182 000-53-160-622 SDI Frame FS513.0 Underfloor BL 0.0 Splice X53-41-183 000-53-900-609 SDI Cabin Windows Surrounding Structure X53-41-184 000-53-160-623 SDI FS409+128 Bulkhead Strap Modfication X53-41-185 000-53-160-624 DVI FS409+128 Bulkhead Strap Modification X53-41-188 000-53-160-625 DVI Keel Beam Cut-out at FS409 +128 X X X53-41-189 000-53-160-626 SDI Keel Beam Cut-out at FS409+128 X X X53-41-190 000-53-900-610 DVI Beacon Light Cut-Outs X53-41-191 000-53-260-616 SDI Frame FS559.00 Inner Cap LH/RH X53-41-192 000-53-260-617 SDI Frame FS409.00 +128 Inner Cap X53-41-193 000-53-160-628 DVI INT Pressure Floor Skin, LH and RH X53-41-194 000-53-160-629 SDI Pressure Floor X53-41-195 000-53-160-630 SDI Pressure Floor Web Fwd & Aft FS460.00 X53-41-196 000-53-160-631 SDI FS409.0 +128 Vertical Beams X53-41-197 000-53-160-632 SDI FS409.0 +128 Vertical Beams X53-41-198 000-53-160-633 DVI FS409.0 +128 Splice Angles STR 21L/R X53-41-199 000-53-160-634 B5341008 SDI FS409.0 +128 Vertical Posts LH and RH X53-41-200 000-53-160-635 DVI FS409.0 +128 Frame Cap Splice Angles X53-41-20-01 000-53-260-504 DVI LH Emergency Exit Cut-out Structure X53-41-20-01 000-53-260-505 DVI RH Emergency Exit Cut-out Structure X53-41-201 000-53-160-636 B5341007 SDI FS559.0 Pressure Bulkhead Web/Cap

Angles X

53-41-24-01 000-53-900-510 DVI LH Longeron T Bracket/Up Surface X53-41-24-01 000-53-900-511 DVI LH Longeron T Bracket/Up Surface X53-41-25-01 000-53-260-502 DVI LH INT Skin Panels, Frames and Stringers X


53-41-26-01 000-53-160-509 DVI LH Wing Attachment Lugs, Frames X53-41-26-01 000-53-160-510 DVI RH Wing Attachment Lugs, Frames X53-41-27-01 000-53-260-502 DVI LH INT Skin Panels, Frames and Stringers X




53-41-29-01 000-53-160-509 DVI LH Wing Attachment Lugs, Frames X53-41-29-01 000-53-160-510 DVI RH Wing Attachment Lugs, Frames X53-41-30-01 000-53-260-502 DVI LH INT Skin Panels, Frames and Stringers X


53-41-31-01 000-53-160-511 DVI LH Side Frame FS513.0 Below Floor X53-41-31-01 000-53-160-512 DVI RH Side, Frame FS513.0 Below Floor X53-41-32-01 000-53-160-500 DVI LH Wing-Attachment Link, FS513.0 X53-41-32-01 000-53-160-501 DVI RH Wing-Attachment Link, FS513.0 X53-41-33-01 000-53-160-507 DVI Overwing Floor Support Beam, FS460.0 X53-41-34-01 000-53-160-513 DVI Pressure Floor Skin Panel Upper Surface X53-41-35-01 000-53-160-514 DVI Pressure Floor Skin Panel Lwr LH Surface X53-41-35-01 000-53-160-515 DVI Pressure Floor Skin Panel Lwr RH Surface X




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CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


53-41-36-01 000-53-160-502 DVI Pressure Floor-Support Beams, X53-41-38-01 000-53-160-508 DVI Pressure Floor Sill Plate/Intercostals X53-41-39-01 000-53-900-510 DVI LH Longeron T Bracket/Up Surface X53-41-39-01 000-53-900-511 DVI LH Longeron T Bracket/Up Surface X53-41-40-01 000-53-160-516 DVI LH Underfloor Longeron Assembly X53-41-40-01 000-53-160-517 DVI RH Underfloor Longeron Assembly X53-41-41-01 000-53-160-503 DVI LH MLG Uplock Structure X53-41-41-01 000-53-160-504 DVI RH MLG Uplock Structure X53-41-42-01 000-53-150-501 DVI Fwd Keel Beam Lugs, Links and Ftgs X53-41-43-01 000-53-900-505 DVI LH Side Seat Rail Structure X53-41-43-01 000-53-900-506 DVI RH Side Seat Rail Structure X53-41-44-01 000-53-170-501 DVI Floor Support Structure X53-41-45-01 000-53-900-505 DVI LH Side Seat Rail Structure X53-41-45-01 000-53-900-506 DVI RH Side Seat Rail Structure X53-41-46-01 000-53-270-501 DVI LH INT Skin Panels, Frames and Stringers X


53-41-47-01 000-53-170-506 DVI INT Skin Panels, Frames and Stringers X53-41-50-01 000-53-170-507 DVI Ext Side Skin Panels X53-41-51-01 000-53-160-505 DVI Aft Keel Beam, FS513.0 to FS559.0 +80 X53-41-51-02 000-53-170-508 DVI Aft Keel Beams X53-41-52-01 000-53-190-500 DVI Aft Lavatory SVC Point Structure X53-41-53-01 000-53-260-500 DVI LH Emergency Exit Stop Ftgs on Fuse X53-41-53-01 000-53-260-501 DVI RH Emergency Exit Stop Ftgs on Fuse X53-61-01-01 000-53-310-501 DVI AFT Pressure Bulkhead Vertical Stiffeners X53-61-02-01 000-53-310-510 DVI AFT Pressure Bulkhead Web Aft Side X53-61-08-01 000-53-170-502 DVI Floor Beam Attach to Pressure Bulkhead X53-61-101 000-53-310-600 DVI AFT Pressure Bulkhead Vert Stiffeners/Web X

53-61-104 000-53-310-601 DVI Longeron to Str 1 Splice at Frame FS718.0 X

53-61-105 000-53-280-600 DVI Aft Pressure Bulkhead Frame Cap X53-61-106 000-53-310-602 DVI Aft Fuse to Vert Stab Drag Angle X53-61-108 000-53-170-600 DVI Floor Beam Attach - Aft Pressure Bulkhead X

53-61-109 000-53-310-603 SDI Pylon to Fuse Attachment Structure X53-61-110 000-53-310-604 SDI ENG Support Beam Upper & Lwr Cap Angles X

53-61-111 000-53-310-605 SDI Skin and Frame Splice at FS672.2 X53-61-112 000-53-310-606 SDI Frame FS625.3 Splice at Str. 9 & Str. 10 X53-61-113 000-53-310-607 DVI Skin Panel at AFT Pressure Bulkhead X53-61-114 000-53-310-608 SDI Eng Support Beam Aft Face X53-61-12-01 000-53-310-508 DVI LH ENG Pylon Splice Angle/Fwd Mount Spar X

53-61-12-01 000-53-310-509 DVI RH ENG Pylon Splice Angle/Fwd Mount Spar X

53-61-140 000-53-280-601 SDI Cargo Door Upper Sill X53-61-141 000-53-280-602 SDI Cargo Door Skin Cut-Out X53-61-142 000-53-310-609 SDI ENG Support Beam Cap Angle Area X53-61-143 000-53-310-610 SDI ENG Support Beam Lwr and Aft Web X53-61-145 000-53-310-612 SDI ENG Support Beam Web Holes/Cap Angles X

53-61-146 000-53-310-613 SDI Eng Supt Beam Lwr & Aft Web Access Holes X

53-61-147a 000-53-280-603 SDI AFT Pressure Bulkhead Fwd Face X




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CRJ 9648

CRJ 9672


53-61-147b 000-53-280-604 DVI AFT Pressure Bulkhead Fwd Face X53-61-148 000-53-310-614 SDI Eng Supt Beam Rpr by GREO-601R-53-61-

345 X

53-61-149 000-53-310-615 SDI ENG Support Beam, FS640.00 Cap Angles X

53-61-150 000-53-280-605 SDI Baggage Door Skin Cut-Outs X53-61-15-01 000-53-170-503 DVI INT Lwr-Fuse Structure X53-61-151 000-53-280-606 SDI Baggage Door Skin Cut-Outs X53-61-152a 000-53-310-616 SDI Eng Support Beam X53-61-152b 000-53-310-617 DVI Eng Support Beam X53-61-153a 000-53-280-607 SDI AFT Pressure Bulkhead Fwd Face53-61-153b 000-53-280-608 052301B DVI AFT Pressure Bulkhead Fwd Face X53-61-154 000-53-280-609 DVI AFTPressure Bulkhead Fwd Face X53-61-16-01 000-53-170-500 DVI Floor Support Structure X53-61-18-01 000-53-170-504 DVI Fwd Side Aft Pressure Bulkhead X53-61-20-01 000-53-280-501 DVI INT Cargo Door Cut-Out Structure X53-61-21-01 000-53-280-500 B0520001 DVI Cargo Door Stop Ftgs X53-61-22-01 000-53-280-503 DVI AFT Pressure Bulkhead Fwd Face X53-61-23-01 000-53-280-504 DVI LH INT Skin Panels, Frames and Stringers X


53-61-24-01 000-53-310-504 DVI Eng Aft Mount Spars at Fuse Frames X53-61-25-01-1 AD2004-10-03A AD041003 DVI Eng Support Beam Structure X53-61-25-01-2 AD2004-10-03A AD041003 DVI Eng Support Beam Structure X53-61-26-01 000-53-310-508 DVI LH ENG Pylon Splice Angle/Fwd Mount Spar X

53-61-26-01 000-53-310-509 DVI RH ENG Pylon Splice Angle/Fwd Mount Spar X

53-61-27-01 000-53-310-507 DVI Lwr Transverse Beam Structure X53-61-29-01 000-53-310-502 DVI Lwr Aft Fuse Interior Structure X53-61-30-01 000-53-310-500 DVI Aft-Equip Compt Door-Cutout INT Structure X

53-61-31-01 000-53-310-511 DVI FS755.0 Frame Structure Fwd Face X53-61-32-01 000-53-280-502 DVI EXT Skin Around Cargo Door Cut-out X53-61-34-01 000-53-310-506 DVI APU Inlet Door Cutout INT Structure X53-61-36-01 000-53-310-503 DVI EXT Skin Around APU Exhaust X53-61-39-01 000-53-900-501 DVI Ext Lwr Skin Panels X53-71-01-01 000-53-350-504 DVI FS755.0 Frame Structure Aft Side X53-71-05-01 000-53-350-502 DVI Vert Stab Front Spar/Fuse Attach Ftg X53-71-07-01 000-53-350-503 DVI FS755.0 Frame Structure Aft Side X53-71-08-01 000-53-350-500 DVI INT Fuse/Stab Section Structure X53-71-10-01 000-53-360-500 DVI VS67.5% Frame Structure Aft Side X53-71-101 000-53-350-600 DVI Frame FS755.0 Above WL125.0 X53-71-102 000-53-350-601 DVI Stringer Extension Attachment X53-71-103 000-53-360-600 DVI Vert Stab Aft Spar and Fuse Frame X53-71-104 000-53-350-602 DVI Vert Stab Mid Spar and Fuse Frame X53-71-105 000-53-350-603 DVI Vert Stab Front Spar Attach Ftgs X53-71-12-01 000-53-350-501 DVI EXT Fuse/Stab Section Skin X54-10-103 000-54-430-602 SDI LH Eng Nacelle Aft Nose Cowl Bulkhead X54-10-103 000-54-440-602 SDI RH Eng Nacelle Aft Nose Cowl Bulkhead X54-10-104 000-54-430-603 DVI LH Eng Nacelle A4 Attachment Ring X54-10-104 000-54-440-603 DVI RH Eng Nacelle A4 Attachment Ring X54-10-105 000-54-430-604 SDI LH Eng Nacelle Pylon Track/Support Ftgs X54-10-105 000-54-440-604 SDI RH Nacelle Pylon Track and Support Ftg X54-10-106 000-54-430-605 SDI LH Eng Pylon Track and Support Ftgs X

This task will not be performed as CHQ has chosen to perform 53-61-153b.




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CRJ 9648

CRJ 9672


54-10-106 000-54-440-605 SDI RH Nacelle Pylon Track and Support Ftg X54-400-01 000-54-410-320 GVI EXT LH Pylon X54-400-02 000-54-410-340 GVI INT LH Pylon Leading Edge X54-400-03 000-54-410-300 GVI INT LH Pylon Mid-Section X54-400-04 000-54-410-360 GVI INT LH Pylon Trailing Edge X54-400-05 000-54-420-320 GVI EXT RH Pylon X54-400-06 000-54-420-340 GVI INT RH Pylon Leading Edge X54-400-07 000-54-420-300 GVI INT RH Pylon Mid-Section X54-400-08 000-54-420-360 GVI INT RH Pylon Trailing Edge X54-51-01-01 000-54-410-500 DVI LH Pylon Front Spar X54-51-01-01 000-54-420-500 DVI RH Pylon Front Spar X54-51-02-02 000-54-410-501 DVI LH Pylon Box EXT Skin X54-51-02-02 000-54-420-501 DVI RH Pylon Box EXT Skin X54-51-03-01 000-54-410-502 DVI LH Pylon Canted Ribs and Drag Braces X54-51-03-01 000-54-420-502 DVI RH Pylon Canted Ribs and Drag Braces X54-51-101 000-54-410-600 SDI LH Eng Pylon Front Spar at FS625.3 X54-51-101 000-54-420-600 SDI RH Eng Pylon Front Spar at FS625.3 X54-51-102 000-54-410-601 DVI LH Eng Pylon Upper and Lwr Skins X54-51-102 000-54-420-601 DVI RH Eng Pylon Upper and Lwr Skins X54-51-103 000-54-410-602 DVI LH Pylon Canted Ribs and Drag Brace X54-51-103 000-54-420-602 DVI RH Pylon Canted Rib and Drag Brace X55-11-01-01 000-55-320-505 DVI Screwjack & Fnt Spar Splice/Bathtub Ftgs X

55-11-02-01 000-55-320-505 DVI Screwjack & Fnt Spar Splice/Bathtub Ftgs X

55-11-03-01 000-55-320-505 DVI Screwjack & Fnt Spar Splice/Bathtub Ftgs X

55-11-04-01 000-55-330-508 DVI INT LH Horiz stab X55-11-04-01 000-55-340-508 DVI INT RH Horiz stab X55-11-05-01 000-55-330-508 DVI INT LH Horiz stab X55-11-05-01 000-55-340-508 DVI INT RH Horiz stab X55-11-05-02 000-55-330-504 DVI LH Elevator Stringers in the PCU Area X55-11-05-02 000-55-340-504 DVI RH Elevator Stringers in the PCU Area X55-11-06-01 000-55-320-506 DVI Aft Spar Splice X55-11-07-01 000-55-330-505 DVI LH Horiz stab Aft Spar Assembly X55-11-07-01 000-55-340-505 DVI RH Horiz stab Aft Spar Assembly X55-11-07-02 000-55-330-508 DVI INT LH Horiz stab X55-11-07-02 000-55-340-508 DVI INT RH Horiz stab X55-11-08-01 000-55-320-507 DVI Aft Centerline Rib (Y-Ftgs) X55-11-09-01 000-55-320-508 DVI Fwd Centerline Rib X55-11-10-01 000-55-320-509 DVI LH Rib BL6.0 X55-11-10-01 000-55-320-510 DVI RH Rib BL6.0 X55-11-102 000-55-320-600 DVI Screwjack Attach Ftgs X55-11-103 000-55-900-600 DVI Front Spar Splice at BL6.0 X55-11-105 000-55-330-600 DVI LH Upper Surface Str. 3 X55-11-105 000-55-340-600 DVI RH Upper Surface Str. 3 X55-11-106 000-55-900-601 DVI Aft Spar Splice/Skin Structure X55-11-110 000-55-320-601 DVI Horiz stab BL6.0 Rib X55-11-115 000-55-330-601 DVI LH Elevator Hinges 1 & 1A Ftgs X55-11-115 000-55-340-601 DVI RH Elevator Hinges 1 and 1A Ftgs X55-11-119 000-55-320-602 DVI Horiz stab Pivot Ftgs X55-11-12-01 000-55-320-511 DVI Upper Skin Splice X55-11-14-01 000-55-320-503 DVI Horiz stab Lwr Skin Splice X55-11-15-01 000-55-330-500 DVI LH Horiz stab Elevator-Hinge Ftgs X55-11-15-01 000-55-340-500 DVI RH Horiz stab Elevator-Hinge Ftgs X55-11-16-02 000-55-330-508 DVI INT LH Horiz stab X




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CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


55-11-16-02 000-55-340-508 DVI INT RH Horiz stab X55-11-17-01 000-55-330-501 DVI LH Horiz stab PCU Attachment Ftgs X55-11-17-01 000-55-340-501 DVI RH Horiz stab PCU Attachment Ftgs X55-11-18-01 000-55-330-506 DVI LH Elevator Flutter Damper Attach Ftgs X55-11-18-01 000-55-340-506 DVI RH Elevator Flutter Damper Attach Ftgs X55-11-19-01 000-55-320-512 DVI Pivot Ftgs X55-11-20-01 000-55-330-508 DVI INT LH Horiz stab X55-11-20-01 000-55-340-508 DVI INT RH Horiz stab X55-11-20-02 000-55-330-502 DVI LH Horiz stab Hinge Ribs X55-11-20-02 000-55-340-502 DVI RH Horiz stab Hinge Ribs X55-11-21-01 000-55-330-508 DVI INT LH Horiz stab X55-11-21-01 000-55-340-508 DVI INT RH Horiz stab X55-11-21-02 000-55-330-503 DVI LH Horiz stab Interior Structure X55-11-21-02 000-55-340-503 DVI RH Horiz stab Interior Structure X55-21-01-01 000-55-330-509 DVI INT LH Elevator X55-21-01-01 000-55-340-509 DVI INT RH Elevator X55-21-03-01 000-55-330-509 DVI INT LH Elevator X55-21-03-01 000-55-340-509 DVI INT RH Elevator X55-21-04-01 000-55-330-507 DVI LH Elevator Hinge Ftgs X55-21-04-01 000-55-340-507 DVI RH Elevator Hinge Ftgs X55-21-05-01 000-55-330-509 DVI INT LH Elevator X55-21-05-01 000-55-340-509 DVI INT RH Elevator X55-21-06-01 000-55-330-509 DVI INT LH Elevator X55-21-06-01 000-55-340-509 DVI INT RH Elevator X55-21-07-01 000-55-330-509 DVI INT LH Elevator X55-21-07-01 000-55-340-509 DVI INT RH Elevator X55-21-101 000-55-330-602 DVI LH Elevator Front Spar Assembly X55-21-101 000-55-340-602 DVI RH Elevator Front Spar Assembly X55-21-107 000-55-330-603 DVI LH Elevator Center and Otbrd Hinge Ftgs X55-21-107 000-55-340-603 DVI RH Elevator Center and Otbd Hinge Ftgs X55-300-01 000-55-320-320 GVI EXT Vertical stab Assembly X55-300-02 000-55-320-340 GVI INT Ram Air Intake and Dorsal Fairing X55-300-03 000-55-320-341 GVI INT Vertical stab Leading Edge X55-300-04 000-55-320-321 GVI INT Vertical stab Assembly X55-300-05 000-55-320-322 GVI INT Vertical stab Tip X55-300-07 000-55-900-320 GVI EXT Horiz stab X55-300-08 000-55-330-340 GVI INT LH Horiz stab Leading Edge X55-300-08 000-55-340-340 GVI INT RH Horiz stab Leading Edge X55-300-09 000-55-900-321 GVI INT Horiz stab X55-300-10 000-55-330-360 GVI INT LH Horiz stab Tip X55-300-10 000-55-340-360 GVI INT RH Horiz stab Tip X55-31-01-01 000-55-320-500 DVI Vert Stab Front Spar Attach-Ftgs X55-31-02-01 000-55-320-513 DVI Front Spar to Fuse Splice Strap X55-31-03-01 000-55-320-514 DVI Front Spar Fwd Face X55-31-05-01 000-55-320-515 DVI Aft Spar Aft Face X55-31-08-01 000-55-320-501 DVI Vert stab Skin Around Access Panel Cutout X

55-31-09-01 000-55-320-516 DVI Vertical stab Stringer Extension Splice X55-31-10-01 000-55-320-517 DVI Canted Rib/Horiz stab Trim Act Pivot Str X55-31-101 000-55-320-603 DVI Front Spar to Fuse Attach Ftgs X55-31-102 000-55-320-604 DVI Front Spar to Fuse Splice Strap X55-31-104 000-55-320-605 DVI Front Spar Attachment at Vertical Rib 1 X55-31-108 000-55-320-606 DVI Access Door Cut-outs X55-31-11-01 000-55-320-502 DVI Horiz stab Pivot Ftgs X55-31-111 000-55-320-607 DVI Vertical stab Pivot Ftgs X55-31-112 000-55-320-608 SDI Trim Actuator Pivot Structure X




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CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


55-31-12-01 000-55-320-517 DVI Canted Rib/Horiz stab Trim Act Pivot Str X55-31-13-01 000-55-320-504 DVI Vertical stab Interior X55-31-14-01 000-55-320-518 DVI Rudder Hinge Ftgs Arms X55-41-02-01 000-55-320-519 DVI Rudder Leading Edge X55-41-03-01 000-55-320-518 DVI Rudder Hinge Ftgs Arms X55-41-04-01 000-55-320-522 DVI Rudder INT Structures X55-41-101 000-55-320-609 GVI Rudder Interface - P/N 601R22014 X X X X55-41-102 000-55-320-610 GVI Rudder Front Spar and Skin-P/N 601R22014 X X X X

57-21-01-01 000-57-900-523 DVI Fwd Face Center Wing Front Spar X57-21-02-01 000-57-510-502 DVI INT LH Side Center Wing X57-21-02-01 000-57-610-502 DVI Internal RH Side Center Wing X57-21-03-01 000-57-510-502 DVI INT LH Side Center Wing X57-21-03-01 000-57-610-502 DVI Internal RH Side Center Wing X57-21-04-01 000-57-900-519 DVI Aft Face Center Wing Aft Spar X57-21-05-01 000-57-510-503 DVI Ext Surface LH Side Center Wing Up Plank X

57-21-05-01 000-57-610-503 DVI Ext Surface RH Side Center Wing Up Plank X

57-21-06-01 000-57-900-520 DVI Ext Surface Center Wing Lwr Plank X57-21-07-01 000-57-510-502 DVI INT LH Side Center Wing X57-21-07-01 000-57-610-502 DVI Internal RH Side Center Wing X57-21-08-01 000-57-510-502 DVI INT LH Side Center Wing X57-21-08-01 000-57-610-502 DVI Internal RH Side Center Wing X57-21-09-01 000-57-510-502 DVI INT LH Side Center Wing X57-21-09-01 000-57-610-502 DVI Internal RH Side Center Wing X57-21-10-01 000-57-520-500 DVI Fwd Face LH Wing Front Spar X57-21-10-01 000-57-620-500 DVI Fwd Face RH Wing Front Spar X57-21-101 000-57-540-603 SDI LH Wing Drain Holes Lwr Plank X57-21-101 000-57-640-603 SDI RH Wing Drain Holes Lwr Wing Plank X57-21-103 000-57-550-600 DVI LH Wing Fnt Spar/Lwr Skin Splice X57-21-103 000-57-650-600 DVI RH Wing Fnt Spar/Lwr Skin Splice X57-21-105 000-57-540-604 DVI LH Wing Lwr Skin, X57-21-105 000-57-640-604 DVI RH Wing Lwr Skin X57-21-107 000-57-510-600 DVI LH Wing Aft Spar Lwr Splice Joint X57-21-107 000-57-610-600 DVI RH Wing Aft Spar Lwr Splice Joint X57-21-110 000-57-520-600 SDI L-Wing Fnt Spar Lwr Splice Joint Lwr Skin X57-21-110 000-57-620-600 SDI R Wing Fnt Spar Lwr Splice Joint/Lwr Skin X

57-21-11-01 000-57-540-501 DVI INT LH Wing X57-21-11-01 000-57-640-501 DVI Internal Right Wing X57-21-111 000-57-540-605 SDI LH Wing Aft Spar Lwr Splice Joint X57-21-111 000-57-640-605 SDI RH Wing Aft Spar Lwr Splice Joint X57-21-112 000-57-510-601 SDI LH Wing Lwr Wing Skin Splice Joints X57-21-112 000-57-610-601 SDI RH Wing Lwr Wing Skin Splice Joints X57-21-113 000-57-550-601 DVI LH Wing Aft Spar Lwr Cap at WS168.0 X57-21-113 000-57-650-601 DVI RH Wing Aft Spar Lwr Cap at WS168.0 X57-21-114 000-57-510-602 DVI LH Wing Front Spar Lwr Cap at BL45.0 X57-21-114 000-57-610-602 DVI RH Wing Front Spar Lwr Cap at BL45.0 X57-21-115 000-57-540-601 SDI LH Wing Lwr Skin Lwr Aft Spar Web X57-21-115 000-57-640-601 SDI RH Wing Lwr Skin aft Spar/Lwr aft Spar Web X

57-21-116 000-57-900-604 SDI Lwr Skin BL0.0 Chordwise Splice X57-21-117 000-57-510-603 SDI LH Wing Electric Boost Pump Access Hole X




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CRJ 9672


57-21-117 000-57-610-603 SDI RH Wing Electric Boost Pump Access Hole X

57-21-118 000-57-510-604 DVI LH Wing Fnt Spar Lwr Splice Joint X57-21-118 000-57-610-604 DVI RH Wing Front Spar Lwr Splice Joint X57-21-119 000-57-510-605 DVI LH Wing to Fuse Attach X57-21-119 000-57-610-605 DVI RH Wing to Fuse Attachment X57-21-120 000-57-510-606 DVI LH Wing to Fuse Attach/MLG Side Brace Ftg X

57-21-120 000-57-610-606 DVI R-Wing Fuse Attach/MLG Side Brace Ftgs X

57-21-12-01 000-57-540-501 DVI INT LH Wing X57-21-12-01 000-57-640-501 DVI Internal Right Wing X57-21-121 000-57-580-600 SDI LH Wing to Inbd Flap Hinge Box Fwd Attach X

57-21-121 000-57-680-600 SDI RH Wing to Inbd Flap Hinge Box Fwd Attach X

57-21-122 000-57-510-607 DVI LH Wing to Fuse Attach X57-21-122 000-57-610-607 DVI RH Wing to Fuse Attachment X57-21-123 000-57-510-608 DVI LH Wing to Fuse Attach X57-21-123 000-57-610-608 DVI RH Wing to Fuse Attachment X57-21-124 000-57-550-602 DVI L-Wing Fnt Spar Lwr Cap and Butt Strap X57-21-124 000-57-650-602 DVI RH Wing Fnt Spar Lwr Cap & Butt Strap X57-21-125 000-57-550-603 SDI L-Wing Aft Spar Lwr Cap and Butt strap X57-21-125 000-57-650-603 SDI RH Wing aftr Spar Lwr Cap & Butt Strap X57-21-127 000-57-590-600 DVI LH Wing to Otbd Flap Hinge Box Fwd Attach X

57-21-127 000-57-690-600 DVI RH Wing to Otbd Flap Hinge Box Fwd Attach X

57-21-128-1 000-57-540-606 SDI LWing Lwr Skin Steel Strap/MLG Trun'n Rib X

57-21-128-1 000-57-640-606 SDI RH Wing Lwr Steel Strap/MLG Trunnion Rib X

57-21-128-2 000-57-540-606 SDI LWing Lwr Skin Steel Strap/MLG Trun'n Rib X

57-21-128-2 000-57-640-606 SDI RH Wing Lwr Steel Strap/MLG Trunnion Rib X

57-21-13-01 000-57-900-500 DVI LH Wing Aft-Spar Aft Face X57-21-13-01 000-57-900-501 DVI RH Wing Aft-Spar Aft Face X57-21-130-1 000-57-540-602 DVI LH Wing Strap X57-21-130-1 000-57-640-602 DVI RH Wing Strap & Surrounding Area X57-21-130-2 000-57-540-602 DVI LH Wing Strap X57-21-130-2 000-57-640-602 DVI RH Wing Strap & Surrounding Area X57-21-134 000-57-550-604 DVI L-Wing Dry Bay Lwr Access Hole Cutout X57-21-134 000-57-650-604 DVI RH Wing Dry Bay Lwr Access Hole Cut-out X

57-21-135 000-57-550-605 DVI L-Wing Lwr Butt Strap/Aft Spar Lwr Cap X57-21-135 000-57-650-605 DVI RH Wing Lwr Butt Strap/aft Spar Lwr Cap X57-21-136 000-57-550-606 DVI LH Wing Aft Spar Splice Joint at WS353.0 X57-21-136 000-57-650-606 DVI RH Wing Aft Spar Splice Joint at WS353.0 X

57-21-138 000-57-570-600 SDI LH Wing Winglet Front/Aft Spar Ftgs X57-21-138 000-57-670-600 SDI RH Wing Winglet Fnt Spar/Aft Spar Ftgs X57-21-139 000-57-540-607 DVI L-Wing Rib Support/Flap Hinge Box Fwd Ftg X

57-21-139 000-57-640-607 DVI R-Wing Rib Supt/Flap Hinge Box Fwd Ftgs X




A1CRJ A2

CRJ A3

CRJ A4

CRJ A5

CRJ A6

CRJ A7

CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


57-21-140 000-57-900-605 SDI LH Wing Rib Support X57-21-140 000-57-900-606 SDI RH Wing Rib Support X57-21-14-01 000-57-540-501 DVI INT LH Wing X57-21-14-01 000-57-640-501 DVI Internal Right Wing X57-21-141 000-57-900-607 SDI LH Wing Lwr Skin Below Flap Hinge Box X57-21-141 000-57-900-608 SDI RH Wing Lwr Skin Below Flap Hinge Box X57-21-142 000-57-550-607 DVI L-Wing Up Skin Access Holes X57-21-142 000-57-650-607 DVI RH Wing Up Skin Holes - Aft & Aux Spar X57-21-143 000-57-550-608 DVI LH Aileron Hinge Ftgs X57-21-143 000-57-650-608 DVI Right Aileron Hinge Ftgs X57-21-145-1 000-57-510-609 SDI LH MLG Mounting Trunnion X57-21-145-1 000-57-610-609 SDI Right MLG Mounting Trunnion X57-21-145-2 000-57-510-609 SDI LH MLG Mounting Trunnion X57-21-145-2 000-57-610-609 SDI Right MLG Mounting Trunnion X57-21-146 000-57-900-609 SDI LH Wing Lwr Plank Access Holes X57-21-146 000-57-900-610 SDI RH Wing Lwr Plank Access Holes X57-21-147 000-57-900-611 SDI LH Wing Lwr Plank Access Holes X57-21-147 000-57-900-612 SDI RH Wing Lwr Plank Access Holes X57-21-148 000-57-900-613 SDI LH Wing Lwr Plank Access Holes X57-21-148 000-57-900-614 SDI RH Wing Lwr Plank Access Holes X57-21-149 000-57-900-615 SDI LH Wing Lwr Plank Access Holes X57-21-149 000-57-900-616 SDI RH Wing Lwr Plank Access Holes X57-21-150 000-57-540-608 SDI L-Wing Drain Hole Lwr Wing Plank-Alt Insp

57-21-150 000-57-640-608 SDI RH Wing Drain Holes Lwr Plank (Alt Insp)57-21-15-01 000-57-540-501 DVI INT LH Wing X57-21-15-01 000-57-640-501 DVI Internal Right Wing X57-21-151 000-57-540-609 SDI LH Wing Aft Lwr Wing Plank at WS148.019 X

57-21-151 000-57-640-609 SDI RH Wing Aft Lwr Wing Plank X57-21-152 000-57-510-610 SDI Boost Pump CutOut LH Wing Lwr Wing

Plank X

57-21-152 000-57-610-610 SDI Boost Pump Cut-Out RH Wing Lwr Wing Plank X

57-21-153 000-57-540-610 SDI LH Wing Aft Lwr Wing Plank at WS148.019 X

57-21-153 000-57-640-610 SDI RH Wing Aft Lwr Wing Plank X57-21-154 000-57-510-611 SDI Fuel Boost Pump CutOut Lwr LH Wing Plank X

57-21-154 000-57-610-611 SDI RH Wing Boost Pump Cut-Out Lwr Wing Plank X

57-21-155 000-57-510-612 SDI LH Main Landing Gear Trunnion Ftgs X57-21-155 000-57-610-612 SDI RH MLG Trunnion Ftgs X57-21-156 000-57-900-619 SDI LH Wing Skin Splice Joints X57-21-156 000-57-900-620 SDI RH Wing Skin Splice Joints X57-21-157 000-57-900-621 SDI Drain Holes in the LH Wing Lwr Plank57-21-157 000-57-900-622 SDI Drain Holes in the RH Wing Lwr Plank57-21-158 000-57-900-623 SDI Drain Holes in the LH Wing Plank57-21-158 000-57-900-624 SDI Drain Holes in the RH Wing Plank57-21-159 000-57-510-613 SDI Boost Pump/Drain Hole CutOut Lwr LH Wing X

57-21-159 000-57-610-613 SDI Boost Pump/Drain Hole Cut-Out LH Wing Lwr X

57-21-16-01 000-57-540-501 DVI INT LH Wing X57-21-16-01 000-57-640-501 DVI Internal Right Wing X57-21-17-01 000-57-550-500 DVI LH Wing Dry Bay Interior Structure X

Not effective CHQ fleetNot effective CHQ fleetNot effective CHQ fleetNot effective CHQ fleet




A1CRJ A2

CRJ A3

CRJ A4

CRJ A5

CRJ A6

CRJ A7

CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


57-21-17-01 000-57-650-500 DVI RH Wing Dry Bay Interior Structure X57-21-18-01 000-57-560-500 DVI Interior Structure Left Wing Plug X57-21-18-01 000-57-660-500 DVI Interior Structure RH Wing Plug X57-21-19-01 000-57-900-502 DVI LH Wing Up Plank Ext Surface X57-21-19-01 000-57-900-503 DVI RH Wing Up Plank Ext Surface X57-21-20-01 000-57-540-502 DVI Ext Surface Lwr LH Wing Plank X57-21-20-01 000-57-640-502 DVI Ext Surface Lwr RH Wing Plank X57-21-21-01 000-57-900-504 DVI Up LH Wing Skin Ext Surface X57-21-21-01 000-57-900-505 DVI Up RH Wing Skin Ext Surface X57-21-22-01 000-57-900-506 DVI Lwr LH Wing Skin Ext Surface X57-21-22-01 000-57-900-507 DVI Lwr RH Wing Skin Ext Surface X57-21-23-01 000-57-540-500 DVI LH Wing Auxiliary Spar Assembly X57-21-23-01 000-57-640-500 DVI RH Wing Auxiliary Spar Assembly X57-21-24-01 000-57-540-503 DVI L-Wing Plank Batt Ribs/Gear Trunnion Ftgs X

57-21-24-01 000-57-640-503 DVI R-Wing Plank, Batt Rib/Gear Trunnion Ftgs X

57-21-25-01-1 000-57-900-512-1 DVI LH MLG Trunnion Strap&Adjacent Wing Skin X

57-21-25-01-2 000-57-900-512-2 DVI RH MLG Trunnion Strap&Adjacent Wing Skin X

57-21-26-01 000-57-540-503 DVI L-Wing Plank Batt Ribs/Gear Trunnion Ftgs X

57-21-26-01 000-57-640-503 DVI R-Wing Plank, Batt Rib/Gear Trunnion Ftgs X

57-21-27-01 000-57-540-504 DVI LH MLG Mounting Ftgs X57-21-27-01 000-57-640-504 DVI Right MLG Mounting Ftgs X57-21-28-01 000-57-900-513 DVI MLG Side Brace Attach Ftgs X57-21-29-01 000-53-150-501 DVI Fwd Keel Beam Lugs, Links and Ftgs X57-21-30-01 000-57-900-514 DVI Aft Spar Bayonet Ftgs X57-21-31-01 000-57-510-501 DVI LH Wing to Fuse Attach Ftgs X57-21-31-01 000-57-610-501 DVI RH Wing to Fuse Attach Ftgs X57-21-32-01 000-57-510-500 DVI LH Wing to Fuse Attach Ftgs X57-21-32-01 000-57-610-500 DVI RH Wing to Fuse Attach Ftgs X57-21-33-01 000-57-510-500 DVI LH Wing to Fuse Attach Ftgs X57-21-33-01 000-57-610-500 DVI RH Wing to Fuse Attach Ftgs X57-21-34-01 000-57-900-508 DVI LH Wing Flap Box Attach Ftgs X57-21-34-01 000-57-900-509 DVI RH Wing Flap Box Attach Ftgs X57-21-35-01 000-57-900-508 DVI LH Wing Flap Box Attach Ftgs X57-21-35-01 000-57-900-509 DVI RH Wing Flap Box Attach Ftgs X57-21-36-01 000-57-550-501 DVI LH Aileron Flutter Damper Attachment Ftgs X

57-21-36-01 000-57-650-501 DVI RH Aileron Flutter Damper Attachment Ftgs X

57-21-37-01 000-57-580-509 DVI Left Wing Jack Ftgs X57-21-37-01 000-57-680-509 DVI Right Wing Jack Ftgs X57-21-38-01 000-57-900-521 DVI LH Wing Lwr Wing Plank Access Holes X57-21-38-01 000-57-900-522 DVI RH Wing Lwr Wing Plank Access Holes X57-31-02-01 000-57-550-502 DVI LH Wing Tip Spars and Ribs X57-31-02-01 000-57-650-502 DVI Right Wing Tip Spars and Ribs X57-500-01 000-57-900-330 GVI External Center Wing Section X57-500-02 000-57-900-320 GVI Internal Center Wing Section X57-500-03 000-57-900-321 GVI External Left Wing Leading Edge X57-500-04 000-57-900-340 GVI Internal Left Wing Leading Edge X57-500-05 000-57-900-321 GVI External Left Wing Leading Edge X57-500-06 000-57-900-340 GVI Internal Left Wing Leading Edge X




A1CRJ A2

CRJ A3

CRJ A4

CRJ A5

CRJ A6

CRJ A7

CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


57-500-07 000-57-900-322 GVI External Left Wing X57-500-08 000-57-900-341 GVI Internal Left Wing Fuel Tank X57-500-09 000-57-900-322 GVI External Left Wing X57-500-10 000-57-900-341 GVI Internal Left Wing Fuel Tank X57-500-11 000-57-550-320 GVI INT LH Wing Outboard Dry Bay X57-500-12 000-57-540-340 GVI INT LH Wing Aft Spar to Auxiliary Spar X57-500-13 000-57-570-320 GVI External Left Wing Tip X57-500-14 000-57-570-340 GVI Internal Left Wing Tip Extension X57-500-16 000-57-900-323 GVI External Left Wing Trailing Edge X57-500-17 000-57-580-320 GVI Internal LH Wing Inboard Trailing Edge X57-500-21 000-57-900-323 GVI External Left Wing Trailing Edge X57-500-22 000-57-590-320 GVI Internal LH Wing OUTBD Trailing Edge X57-500-27 000-57-590-321 GVI Internal Left Aileron Shrouds X57-51-01-01 000-57-900-510 DVI LH Wing Gnd/Flt Spoiler & Spoileron Hinge X

57-51-01-01 000-57-900-511 DVI RH Wing Gnd/Flt Spoiler & Spoileron Hinge X

57-51-02-01 000-57-900-510 DVI LH Wing Gnd/Flt Spoiler & Spoileron Hinge X






57-51-05-01 000-57-590-500 DVI Left Wing Aileron Hinge Ftgs X57-51-05-01 000-57-690-500 DVI Right Wing Aileron Hinge Ftgs X57-52-02-01 000-57-580-500 DVI Left Inboard Flap Lwr Skin X57-52-02-01 000-57-680-500 DVI Right Inboard Flap Lwr Skin X57-52-03-01 000-57-580-510 DVI Left Inboard Flap Front Spar X57-52-03-01 000-57-680-510 DVI Right Inboard Flap Front Spar X57-52-04-01 000-57-580-505 DVI LH Inbd Flap Vane Actuator Carriages X57-52-04-01 000-57-680-505 DVI RH Inbd Flap Vane Act Carriages/Support X57-52-06-01 000-57-580-506 DVI LH Inboard Flap Hinge Support Ribs X57-52-06-01 000-57-680-506 DVI RH Inboard Flap Hinge Support Ribs X57-52-07-01 000-57-580-507 DVI LH Inboard Flap Hinge Lug Plates X57-52-07-01 000-57-680-507 DVI RH Inboard Flap Hinge Lug Plates X57-52-08-01 000-57-580-504 DVI Left Inboard Flap Hinge Arms X57-52-08-01 000-57-680-504 DVI Right Inboard Flap Hinge Arms X57-52-105 000-57-580-601 DVI LH Inbd Flap Front Spar/Intercostal Spar X57-52-105 000-57-680-601 DVI RH Inbd Flap Fnt Spar & Intercostal Spar X57-52-106 000-57-580-602 DVI Left Inboard Flap Hinge Ribs X57-52-106 000-57-680-602 DVI Right Inboard Flap Hinge Ribs X57-52-107 000-57-580-603 DVI Left Inboard Flap Lug Plates X57-52-107 000-57-680-603 DVI Right Inboard Flap Lug Plates X57-52-108 000-57-580-604 DVI Left Inboard Flap Hinge Arms X57-52-108 000-57-680-604 DVI Right Inboard Flap Hinge Arms X57-52-112 000-57-580-605 DVI LH Inboard Flap Upper and Lwr Skin X57-52-112 000-57-680-605 DVI RH Inboard Flap Upper and Lwr Skin X57-52-113 000-57-580-606 DVI Left Inboard Flap Hinge Arms X57-52-113 000-57-680-606 DVI Right Inboard Flap Hinge Arms X




A1CRJ A2

CRJ A3

CRJ A4

CRJ A5

CRJ A6

CRJ A7

CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


57-52-114 000-57-580-607 DVI LH INBD Flap Vane Actuator Tube Assembly X

57-52-114 000-57-680-607 DVI RH INBD Flap Vane Actuator Tube Assembly X

57-52-118 000-57-580-608 SDI Left Inboard Flap Vane Skin X57-52-118 000-57-680-608 SDI Right Inboard Flap Vane Skin X57-52-119 000-57-580-609 SDI LH Inbd Flap Vane Mounting Structure X57-52-119 000-57-680-609 SDI RH Inbd Flap Vane Mounting Structure X57-52-14-01 000-57-580-501 DVI LH INBD Flap Vane Actuator Sliding Beams X

57-52-14-01 000-57-680-501 DVI RH INBD Flap Vane Actuator Sliding Beams X

57-52-15-01 000-57-580-505 DVI LH Inbd Flap Vane Actuator Carriages X57-52-15-01 000-57-680-505 DVI RH Inbd Flap Vane Act Carriages & Support X

57-52-17-01 000-57-580-503 DVI Left Inboard Flap Vane Skin X57-52-17-01 000-57-680-503 DVI Right Inboard Flap Vane Skin X57-52-19-01 000-57-580-511 DVI LH Inboard Flap Vane Mounting Structure X57-52-19-01 000-57-680-511 DVI RH Inboard Flap Vane Mounting Structure X57-52-20-01 000-57-580-512 DVI LH Inboard Flap Internal Structure X57-52-20-01 000-57-680-512 DVI RH Inboard Flap Internal Structure X57-53-04-01 000-57-590-510 DVI LH Outboard Flap Vane Mounts & Structure X

57-53-04-01 000-57-690-510 DVI RH Outboard Flap Vane Mounts & Structure X

57-53-05-01 000-57-590-511 DVI LH Otbd Flap Hinge Int Support Structure X57-53-05-01 000-57-690-511 DVI RH Otbd Flap Hinge Int Support Structure X57-53-07-01 000-57-590-512 DVI LH Outboard Flap Hinge Lug Ftgs X57-53-07-01 000-57-690-512 DVI RH Outboard Flap Hinge Lug Ftgs X57-53-10-01 000-57-590-509 DVI LH OUTBD Flap INBD Hinge Arm Assembly X

57-53-10-01 000-57-690-509 DVI RH OUTBD Flap INBD Hinge Arm Assembly X

57-53-102 000-57-590-601 DVI LH Outboard Flap Upper and Lwr Skin X57-53-102 000-57-690-601 DVI RH Outboard Flap Upper and Lwr Skin X57-53-103 000-57-590-602 SDI Left Outboard Flap Front Spar X57-53-103 000-57-690-602 SDI Right Outboard Flap Front Spar X57-53-104 000-57-590-603 DVI LH Outboard Flap Vane Support Structure X57-53-104 000-57-690-603 DVI RH Outboard Flap Vane Support Structure X57-53-105 000-57-590-604 DVI LH Otbd Flap Vane Mount Lug/Nose Riblet X

57-53-105 000-57-690-604 DVI R Otbd Flap Vane Mounting Lug/Nose Riblet X

57-53-106 000-57-590-605 DVI LH Outboard Flap Hinge Support Structure X57-53-106 000-57-690-605 DVI RH Outboard Flap Hinge Support Structure X

57-53-107 000-57-590-606 DVI LH Otbd Flap Nose Riblet at Flap Arm X57-53-107 000-57-690-606 DVI RH Otbd Flap Nose Riblet at Flap Arm X57-53-110 000-57-590-607 SDI LH Otbd Flap Intercostal Spar Machinings X57-53-110 000-57-690-607 SDI RH Otbd Flap Intercostal Spar Machinings X57-53-114 000-57-590-608 DVI Left Outboard Flap Hinge Arms X57-53-114 000-57-690-608 DVI Right Outboard Flap Hinge Arms X57-53-118 000-57-590-609 SDI LH Otbd Flap Hinge Box to Flap Attach X57-53-118 000-57-690-609 SDI RH Otbd Flap Hinge Box to Flap Attachment X

57-53-12-01 000-57-590-504 DVI LH Otbd Flap Center Hinge Lug Ftgs/Arm X




A1CRJ A2

CRJ A3

CRJ A4

CRJ A5

CRJ A6

CRJ A7

CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


57-53-12-01 000-57-690-504 DVI R Otbd Flap Center Hinge Lug Ftgs & Arm X57-53-122 000-57-590-610 DVI Left Outboard Flap Vane X57-53-122 000-57-690-610 DVI Right Outboard Flap Vane X57-53-125 TBD Composite outboard flap components X57-53-13-01 000-57-590-504 DVI LH Otbd Flap Center Hinge Lug Ftgs/Arm X57-53-13-01 000-57-690-504 DVI R Otbd Flap Center Hinge Lug Ftgs & Arm X57-53-15-01 000-57-590-511 DVI LH Otbd Flap Hinge Int Support Structure X57-53-15-01 000-57-690-511 DVI RH Otbd Flap Hinge Int Support Structure X57-53-17-01 000-57-590-512 DVI LH Outboard Flap Hinge Lug Ftgs X57-53-17-01 000-57-690-512 DVI RH Outboard Flap Hinge Lug Ftgs X57-53-20-01 000-57-590-505 DVI LH OUTBD Flap OUTBD Hinge Arm

Assembly X

57-53-20-01 000-57-690-505 DVI RH OUTBD Flap OUTBD Hinge Arm Assembly X

57-53-24-01 000-57-590-510 DVI LH Outboard Flap Vane Mounts & Structure X

57-53-24-01 000-57-690-510 DVI RH Outboard Flap Vane Mounts & Structure X

57-53-25-01 000-57-590-513 DVI LH Outboard Flap Internal Structure X57-53-25-01 000-57-690-513 DVI RH Outboard Flap Internal Structure X57-54-01-01 000-57-590-507 DVI Left Inboard Flap Hinge Boxes X57-54-01-01 000-57-690-507 DVI Right Inboard Flap Hinge Boxes X57-54-02-01 000-57-590-508 DVI Left Outboard Flap Hinge Boxes X57-54-02-01 000-57-690-508 DVI Right Outboard Flap Hinge Boxes X57-54-103 000-57-580-610 B5754001 SDI LH Inbd Flap Hinge Boxes X57-54-103 000-57-680-610 B5754001 SDI RH Inbd Flap Hinge Boxes X57-54-105 000-57-590-611 SDI LH Otbd Flap Hinge Boxes X57-54-105 000-57-690-611 SDI RH Otbd Flap Hinge Boxes X57-600-01 000-57-900-330 GVI External Center Wing Section X57-600-02 000-57-900-320 GVI Internal Center Wing Section X57-600-03 000-57-900-324 GVI External Right Wing Leading Edge X57-600-04 000-57-900-342 GVI Internal Right Wing Leading Edge X57-600-05 000-57-900-324 GVI External Right Wing Leading Edge X57-600-06 000-57-900-342 GVI Internal Right Wing Leading Edge X57-600-07 000-57-900-325 GVI External Right Wing X57-600-08 000-57-900-343 GVI Internal Right Wing Fuel Tank X57-600-09 000-57-900-325 GVI External Right Wing X57-600-10 000-57-900-343 GVI Internal Right Wing Fuel Tank X57-600-11 000-57-650-320 GVI Internal RH Wing Outboard Dry Bay X57-600-12 000-57-640-340 GVI Int RH Wing Aft Spar to Aux Spar X57-600-13 000-57-670-320 GVI External Right Wing Tip X57-600-14 000-57-670-340 GVI Internal Right Wing Tip Extension X57-600-16 000-57-900-326 GVI External Right Wing Trailing Edge X57-600-17 000-57-680-320 GVI Internal RH Wing Inboard Trailing Edge X57-600-21 000-57-900-326 GVI External Right Wing Trailing Edge X57-600-22 000-57-690-320 GVI Internal RH Wing OUTBD Trailing Edge X57-600-27 000-57-690-321 GVI Internal Right Aileron Shrouds X57-61-01-01 000-57-590-514 DVI Left Aileron Center Ftgs X57-61-01-01 000-57-690-514 DVI Right Aileron Center Ftgs X57-61-04-01 000-57-590-506 DVI Left Aileron Front Spar X57-61-04-01 000-57-690-506 DVI Right Aileron Front Spar X57-61-05-01 000-57-590-515 DVI Left Aileron Internal Structure X57-61-05-01 000-57-690-515 DVI Right Aileron Internal Structure X57-61-06-01 000-57-590-503 DVI Left Aileron Hinge Ftgs X57-61-06-01 000-57-690-503 DVI Right Aileron Hinge Ftgs X57-61-101 000-57-590-612 DVI Left Aileron Center Ftgs X




A1CRJ A2

CRJ A3

CRJ A4

CRJ A5

CRJ A6

CRJ A7

CRJ A8

CRJ A9

CRJ A10

CRJ C1

CRJ C2

CRJ C3

CRJ C4

CRJ C5

CRJ 24

CRJ 48

CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


57-61-101 000-57-690-612 DVI Right Aileron Center Ftgs X57-61-102 000-57-590-613 DVI Left Aileron Lwr Skin Panel X57-61-102 000-57-690-613 DVI Right Aileron Lwr Skin Panel X57-61-104 000-57-590-614 DVI Left Aileron Front Spar X57-61-104 000-57-690-614 DVI Right Aileron Front Spar X57-61-105 000-57-590-615 DVI Left Aileron Internal Structure X57-61-105 000-57-690-615 DVI Right Aileron Internal Structure X57-61-106 000-57-590-616 DVI LH Aileron Hinge Ftgs/BackUp Structure X X X X57-61-106 000-57-690-616 DVI RH Aileron Hinge Ftgs/Back-Up Structure X X X X57-61-107 000-57-590-617 DVI of the Left Aileron Upper and Lwr Skin X X X X57-61-107 000-57-690-617 DVI of the RH Aileron Upper and Lwr Skin X X X X57-61-108 000-57-590-618 B5761001 SDI LH Aileron Front Spar & Front Spar Splice X57-61-108 000-57-690-618 B5761002 SDI RH Aileron Front Spar & Front Spar Splice X57-61-109 000-57-590-619 B5761003 SDI Left Aileron Side Hinge Pins X57-61-109 000-57-690-619 B5761004 SDI Right Aileron Side Hinge Pins X57-71-01-01 000-57-580-502 DVI LH Wing Gnd Spoiler Hinge & structure X57-71-01-01 000-57-680-502 DVI RH Wing Gnd Spoiler Hinge Rib Spar & Skin X

57-71-02-01 000-57-580-502 DVI LH Wing Gnd Spoiler Hinge & structure X57-71-02-01 000-57-680-502 DVI RH Wing Gnd Spoiler Hinge Rib Spar & Skin X



57-73-01-01 000-57-590-501 DVI LH Wing Flt Spoiler Hinge Ftgs X57-73-01-01 000-57-690-501 DVI R-Wing Flt Spoiler Hinge Ftgs Spar Skin X57-73-02-01 000-57-590-501 DVI LH Wing Flt Spoiler Hinge Ftgs X57-73-02-01 000-57-690-501 DVI R Wing Flt Spoiler Hinge Ftgs Spar Skin X57-74-01-01 000-57-590-502 DVI Left Wing Spoileron Assembly X57-74-01-01 000-57-690-502 DVI Right Wing Spoileron Assembly X71-12-00-03 000-71-430-105 DVI LH ENG Core-Cowl Blowout Door X71-12-00-03 000-71-440-105 DVI RH ENG Core-Cowl Blowout Door X71-16-00-03 000-71-430-102 DVI Left Eng Fwd Core Cowl X71-16-00-03 000-71-440-102 DVI Right Eng Fwd Core Cowl X71-16-00-07 000-71-430-102 DVI Left Eng Fwd Core Cowl X71-16-00-07 000-71-440-102 DVI Right Eng Fwd Core Cowl X71-16-00-09 000-71-430-102 DVI Left Eng Fwd Core Cowl X71-16-00-09 000-71-440-102 DVI Right Eng Fwd Core Cowl X71-21-00-01 TBD DVI Fwd Eng Mount / Yoke / Link Assembly X71-21-101 000-71-430-600 SDI Left Eng Mount Yoke Ftgs X71-21-101 000-71-440-600 SDI Right Eng Mount Yoke Ftgs X71-21-102 000-71-430-601 SDI Left Eng Mount Thrust Ftgs X71-21-102 000-71-440-601 SDI Right Eng Mount Thrust Ftgs X71-21-103 000-71-430-602 SDI LH ENG Up Link Yoke Ftgs at FS625.3 X71-21-103 000-71-440-602 SDI RH ENG Up Link Yoke Ftgs at FS625.3 X71-21-104 000-71-430-603 SDI Left Eng Mount Shaft X71-21-104 000-71-440-603 SDI Right Eng Mount Shaft X71-22-00-01 TBD DVI Aft Eng Mount & Components X71-31-00-01 000-71-900-101 GVI LH ENG Nacelle/Pylon Firewall X71-31-00-01 000-71-900-102 GVI RH ENG Nacelle/Pylon Firewall X71-400-01 000-71-430-300 GVI External Left Eng Nacelle X71-400-02 000-71-430-320 GVI Internal Left Eng Nose Cowl X71-400-03 000-71-430-330 GVI Internal LH ENG Nose Access Cowl X




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71-400-04 000-71-430-331 GVI Internal LH ENG Reverser Torque Box X71-400-05 000-71-430-340 GVI Internal LH ENG Translating Cowl X71-400-06 000-71-430-301 GVI Internal LH ENG Upper & Lwr Core Cowls X71-400-07 000-71-430-321 GVI Internal LH ENG Tail Pipe Fairing X71-400-08 000-71-440-300 GVI External Right Eng Nacelle X71-400-09 000-71-440-320 GVI Internal Right Eng Nose Cowl X71-400-10 000-71-440-332 GVI Internal RH ENG Nose Access Cowl X71-400-11 000-71-440-331 GVI Internal RH ENG Reverser Torque Box X71-400-12 000-71-440-341 GVI Internal RH ENG Translating Cowl X71-400-13 000-71-440-301 GVI Internal RH ENG Upper & Lwr Core Cowls X71-400-14 000-71-440-321 GVI Internal RH ENG Tail Pipe Fairing X71-51-00-02 TBD DVI Eng Core Cowl Master Harness A (Red) X71-51-00-04 TBD DVI Eng Core Cowl Master Harness B (Violet) X71-52-00-02 TBD DVI Eng Nose Cowl Accessory Harness (orange) X

71-61-00-01 000-71-430-001 GVI of the LH ENG Nose Inlet-Cowl Assembly X X71-61-00-01 000-71-440-001 GVI of the RH ENG Nose Inlet-Cowl Assembly X X71-61-00-05 000-71-430-106 GVI LH ENG Nose Inlet-Cowl Assembly X71-61-00-05 000-71-440-106 GVI RH ENG Nose Inlet-Cowl Assembly X71-61-00-07 000-71-430-107 DVI nacelle nose cowl fasteners for security X71-61-00-07 000-71-440-107 DVI nacelle nose cowl fasteners for security X72-21-00-01 TBD DIS Eng Fan Disk X72-21-00-03 000-72-430-001 Inspection of the Left Eng Inlet Fan X X X X X X X X X X72-21-00-03 000-72-440-001 Inspection of the Right Eng Inlet Fan X X X X X X X X X X72-21-00-05 000-72-430-001 Inspection of the Left Eng Inlet Fan X X X X X X X X X X72-21-00-05 000-72-440-001 Inspection of the Right Eng Inlet Fan X X X X X X X X X X72-21-00-07 TBD DIS Eng Fan Fwd Shaft X72-21-00-09 LC2 DVI of ENG master chip detector indicator X72-22-00-01 TBD DIS Eng Fan Drive Shaft X72-23-00-01 000-72-430-100 DVI LH ENG Fan Case and Fwd ENG Mounts X72-23-00-01 000-72-440-100 DVI RH ENG Fan Case and Fwd ENG Mounts X72-23-00-03 000-72-430-100 DVI LH ENG Fan Case and Fwd ENG Mounts X72-23-00-03 000-72-440-100 DVI RH ENG Fan Case and Fwd ENG Mounts X72-23-00-07 000-72-430-001 Inspection of the Left Eng Inlet Fan X X X X X X X X X X72-23-00-07 000-72-440-001 Inspection of the Right Eng Inlet Fan X X X X X X X X X X72-31-00-01 000-72-430-101 DVI Left Eng Front Frame X72-31-00-01 000-72-440-101 DVI Right Eng Front Frame X72-32-00-01 000-72-430-102 DVI L Eng VG Act Assemblies Unison Rings/Link X

72-32-00-01 000-72-440-102 DVI R Eng VG Act Assemblies Unison Rings/Link X

72-32-00-03 000-72-430-107 B7232001 Boro L-Eng Comp Blade,Var Guide Vane,Stat Vane X

72-32-00-03 000-72-440-107 B7232001 Boro R-Eng Comp Blade,Var Guide Vane,Stat Vane X

72-32-00-05 000-12-430-001 LUB LH Eng Variable Guide Vanes X X X X X72-32-00-05 000-12-440-001 LUB RH Eng Variable Guide Vanes X X X X X72-33-00-01 000-72-430-107 B7232001 Boro L-Eng Comp Blade,Var Guide Vane,Stat

Vane X

72-33-00-01 000-72-440-107 B7232001 Boro R-Eng Comp Blade,Var Guide Vane,Stat Vane X

72-33-00-03-1 TBD DIS ENG Compressor Rotor Stage 1 Disc X72-33-00-03-2 TBD DIS ENG Compressor Rotor Fwd Shaft X72-33-00-03-3 TBD DIS ENG Compressor Rotor Stage 2 Disc X72-33-00-03-4 TBD DIS Eng Comp Rotor Stage 3-8 Rotor Spool X72-33-00-03-5 TBD DIS Eng Comp Rotor Stage 10-14 Rotor Spool X




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72-33-00-03-6 TBD DIS ENG Compressor Rotor Aft Shaft CDP Seal X

72-33-00-03-7 TBD DIS ENG Compressor Rotor Aft Shaft X72-33-00-03-8 TBD DIS ENG Compressor Rotor Stage 9 Disc X72-41-00-03 000-72-430-002 Inspection of the Left Eng X X X X X X X X X X72-41-00-03 000-72-440-002 Inspection of the Right Eng X X X X X X X X X X72-42-00-01 000-72-430-708 B7242001 Boro L-Eng Comb Liner, 1 Turb nozzle/Injector X72-42-00-01 000-72-440-708 B7242002 Boro R-Eng Comb Liner, 1 Turb nozzle/Injector X72-42-00-03 000-72-430-708 B7242001 Boro L-Eng Comb Liner, 1 Turb nozzle/Injector X72-42-00-03 000-72-440-708 B7242002 Boro R-Eng Comb Liner, 1 Turb nozzle/Injector X72-43-00-01 000-72-430-002 Inspection of the Left Eng X X X X X X X X X X72-43-00-01 000-72-440-002 Inspection of the Right Eng X X X X X X X X X X72-44-00-01 000-72-430-106 DVI Left Eng Aft Mount X72-44-00-01 000-72-440-106 DVI Right Eng Aft Mount X72-50-00-11 000-72-430-003 SDI of the Left Eng C-Sump Drain X X X X X X X X X X72-50-00-11 000-72-440-003 SDI of the Right Eng C-Sump Drain X X X X X X X X X X72-52-00-01 000-72-430-700 B7252001 Boro LH ENG HPT Stages 1 & 2 Rotor Blades X72-52-00-01 000-72-440-700 B7252002 Boro RH ENG HPT Stages 1 & 2 Rotor Blades X72-52-00-03-1 TBD DIS ENG High Press Turbine Rotor Stage 1 Disc X

72-52-00-03-2 TBD DIS ENG High Press Turbine Rotor Stage 2 Disc X

72-52-00-03-3 TBD DIS Eng HPT Rotor Balance Piston Seal X72-52-00-03-4 TBD DIS ENG High Press Turbine Rotor HPT Shaft X72-52-00-03-5 TBD DIS Eng HPT Rotor Outer Torque Coupling X72-52-00-03-6 TBD DIS Eng HPT Rotor Inner Torque Coupling X72-53-00-01 000-72-430-109 DVI Left Eng X72-53-00-01 000-72-440-109 DVI Right Eng X72-55-00-03-1 TBD DIS Eng LPT Rotor Turbine Aft Shaft X72-55-00-03-2 TBD DIS ENG Low Press Turbine Rotor Stage 3 Disc X

72-55-00-03-3 TBD DIS Eng LPT Rotor Stage 3/4 Disc X72-55-00-03-4 TBD DIS ENG Low Press Turbine Rotor Stage 4 Disc X

72-55-00-03-5 TBD DIS Eng LPT Rotor Stage 4/5 Disc X72-55-00-03-6 TBD DIS ENG Low Press Turbine Rotor Stage 5 Disc X

72-55-00-03-7 TBD DIS Eng LPT Rotor Stage 5/6 Seal X72-55-00-03-8 TBD DIS ENG Low Press Turbine Rotor Stage 6 Disc X

72-55-00-03-9 TBD DIS ENG Low Press Turbine Rotor Drive Cone X72-56-00-01 000-72-430-002 Inspection of the Left Eng X X X X X X X X X X72-56-00-01 000-72-440-002 Inspection of the Right Eng X X X X X X X X X X72-60-00-01 000-72-430-002 Inspection of the Left Eng X X X X X X X X X X72-60-00-01 000-72-440-002 Inspection of the Right Eng X X X X X X X X X X72-60-00-03 000-72-430-109 DVI Left Eng X72-60-00-03 000-72-440-109 DVI Right Eng X73-11-01-01 000-73-430-120 DVI Left Eng Fuel Pump Housing X73-11-01-01 000-73-440-120 DVI Right Eng Fuel Pump Housing X73-11-03-01 000-73-430-002 DIS Left Eng Fuel Filter Element X X X73-11-03-01 000-73-440-002 DIS Right Eng Fuel Filter Element X X X73-11-03-03 000-73-430-001 VCK of LH ENG Fuel Filter ByPax Indicator X X X X X73-11-03-03 000-73-440-001 VCK of RH ENG Fuel Filter ByPax Indicator X X X X X73-11-09-01 000-73-430-003 GVI of the Left Eng Fuel Manifold X X X73-11-09-01 000-73-440-003 GVI of the Right Eng Fuel Manifold X X X73-11-11-01 000-72-430-708 B7242001 Boro L-Eng Comb Liner, 1 Turb nozzle/Injector X




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73-11-11-01 000-72-440-708 B7242002 Boro R-Eng Comb Liner, 1 Turb nozzle/Injector X73-21-01-01 000-73-430-700 B0520002 DVI of the Left Eng Main Fuel Control X73-21-01-01 000-73-440-700 B0520002 DVI of the Right Eng Main Fuel Control X73-21-01-03 000-73-430-101 GVI LH ENG Brown Electrical Cable X73-21-01-03 000-73-440-101 GVI RH ENG Brown Electrical Cable X73-21-01-09 000-73-430-102 DVI Left Eng Main Fuel Control X73-21-01-09 000-73-440-102 DVI Right Eng Main Fuel Control X76-11-00-01 000-76-430-150 GVI LH ENG Throttle quad and control cable X76-11-00-01 000-76-440-150 GVI RH ENG Throttle quad and control cable X76-11-00-03 000-76-900-100 FNC ACSU Throttle Quadrant Microswitches X76-11-00-05 000-76-430-121 FNC the LH ENG Throttle Control System X76-11-00-05 000-76-440-121 FNC the RH ENG Throttle Control System X76-11-00-09 000-76-900-101 FNC the Throttle Lockout System X76-11-00-11 000-76-430-700 FNC LH ENG Throttle control gearbox X76-11-00-11 000-76-440-700 FNC RH ENG Throttle control gearbox X76-11-00-13 TBD SDI Throttle gear box for gear tooth wear X78-11-00-01 000-78-430-120 DVI Left Eng Exhaust 0zzle X78-11-00-01 000-78-440-120 DVI Right Eng Exhaust 0zzle X78-30-00-03 000-78-900-700 B0520002 FNC the Eng Thrust Reverser System X78-30-00-05 000-12-430-700 B0520002 LUB LH Eng Thrust Reverser X78-30-00-05 000-12-440-700 B0520002 LUB RH Eng Thrust Reverser X78-30-00-07 000-78-430-001 DVI of LH ENG Reverser Sys Components X X78-30-00-07 000-78-440-001 DVI of RH ENG Reverser Sys Components X X78-30-00-09 000-12-430-002 LUB LH TR Tracks and Ballscrew Actuators X X X X X X X X X X78-30-00-09 000-12-440-002 LUB RH TR Tracks and Ballscrew Actuators X X X X X X X X X X79-11-01-01 000-79-430-001 DVI of the Left Eng Oil Tank Assembly X X X79-11-01-01 000-79-440-001 DVI of the Right Eng Oil Tank Assembly X X X79-11-01-03 LC1 Service the Eng oil tank X79-12-00-01 LC1 Service the Eng oil replenishment tank X79-21-01-01 000-79-430-701 B0520002 DVI of LH ENG C-Sump Scavenge Screen Ftgs X

79-21-01-01 000-79-440-701 B0520002 DVI of RH ENG C-Sump Scavenge Screen Ftgs X

79-21-05-01 000-79-310-001 VCK of the ENG Oil Filter ByPax Indicator X X X X X79-21-05-03 000-79-430-700 FNC LH ENG Oil-Filter ByPass-Sensor X79-21-05-03 000-79-440-700 FNC RH ENG Oil-Filter ByPass-Sensor X79-21-05-05 000-79-430-002 DIS Left Eng Oil Filter X X X79-21-05-05 000-79-440-002 DIS Right Eng Oil Filter X X X79-21-09-01 000-79-900-100 OPC LH and RH ENG Master Chip Detectors X80-11-00-01 000-80-430-002 DVI LH ENG ATS Mag Drain Plug & oil change X X X X X

80-11-00-01 000-80-440-002 DVI RH ENG ATS Mag Drain Plug & oil change X X X X X

80-11-00-03 000-80-430-002 DVI LH ENG ATS Mag Drain Plug & oil change X X X X X

80-11-00-03 000-80-440-002 DVI RH ENG ATS Mag Drain Plug & oil change X X X X X

80-11-00-05 000-80-430-001 VCK of LH ENG ATS Oil Level X X X X X X X X X X80-11-00-05 000-80-440-001 VCK of RH ENG ATS Oil Level X X X X X X X X X Xa/c Weigh 000-08-011-000 B0811001 CRJ 200 Weighing Procedures XAD 2002-03-14 AD2002-03-14 AD020314 To find and fix cracking of the left and right lower

wing planks, which could result in reduced structural integrity of the wing

X




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AD 2002-16-02 AD2002-16-02 Part Master File

To prevent failure of key components of the horizontal stabilizer trim actuators (HSTAs), which could result in loss of horizontal trim control and consequent reduced controllability of the airplane

X

AD 2003-09-04 R1 AD2003-09-04B 030904B To detect and correct in a timely manner fatigue cracks of the pressure floor skin of the center fuselage at fuselage stations 460 and 513, which could result in failure of the pressure floor skin and consequent rapid decompression of the airplane during flight

X

AD 2003-11-11 AD2003-11-11A-1 031111A1 To prevent failure of the MLG main fittings, which could result in collapse of the MLG upon landing X

AD 2003-11-11 AD2003-11-11A-2 031111A2 To prevent failure of the MLG main fittings, which could result in collapse of the MLG upon landing X

AD 2003-11-11 AD2003-11-11B-1 031111B1 To prevent failure of the MLG main fittings, which could result in collapse of the MLG upon landing X

AD 2003-11-11 AD2003-11-11B-2 031111B2 To prevent failure of the MLG main fittings, which could result in collapse of the MLG upon landing X

AD 2003-11-20 AD2003-11-20 AD031120 To prevent temporary loss of braking action due to the freezing of moisture on the input plunger of the brake control valve during steep descent X

AD 2003-20-03 000-53-160-604 AD032003 To detect and correct, in a timely manner, fatigue cracks in the vertical beams of the pressure bulkheads at fuselage stations 409+128 and 559, which could result in the reduced structural integrity of the airplane,

X

AD 2004-10-03 AD2004-10-03A AD041003 To prevent failure of the engine support beam (ESB), a principal structural element, which could result in reduced structural integrity of the airplane X

AD 2004-14-16 AD superceded by AD 2007-03-19AD 2004-14-16 AD superceded by AD 2007-03-19AD 2004-14-16 AD superceded by AD 2007-03-19AD 2004-14-16 AD superceded by AD 2007-03-19AD 2004-20-09 AD superceded by AD 2007-01-07AD 2004-20-09 AD superceded by AD 2007-01-07AD 2004-20-09 AD superceded by AD 2007-01-07AD 2004-20-09 AD superceded by AD 2007-01-07AD 2004-22-08 AD2004-22-08A 042208A To prevent disconnection of an air supply duct,

which, if combined with failure of a bulkhead check valve, could result in rapid depressurization of the airplane

X

AD 2005-03-13 AD2005-03-13 AD050313 This AD was prompted by reports indicating that the links of the aileron power control unit (PCU) have failed. We are issuing this AD to prevent failure of both links of the aileron PCU, which could result in reduced lateral control of the airplane.

X




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AD 2005-06-04 AD2005-06-04-1 050604-1 This AD was prompted by numerous failures of the engine throttle control gearbox, some of which resulted in an in-flight engine shutdown. We are issuing this AD to prevent excessive wear of the gearboxes and subsequent movement or jamming of the engine throttle; movement of the throttle towards the idle position brings it close to the fuel shut-off position, which could result in an in- flight engine shutdown.

X

AD 2005-06-04 AD2005-06-04-2 050604-2 This AD was prompted by numerous failures of the engine throttle control gearbox, some of which resulted in an in-flight engine shutdown. We are issuing this AD to prevent excessive wear of the gearboxes and subsequent movement or jamming of the engine throttle; movement of the throttle towards the idle position brings it close to the fuel shut-off position, which could result in an in- flight engine shutdown.

X

AD 2005-10-10 AD2005-10-10 AD051010 This AD is prompted by a report of a potential failure of the horizontal stabilizer trim actuator (HSTA) secondary nut in conjunction with a latent failure of the HSTA primary load path discovered during sampling program activities. We are issuing this AD to detect and correct latent failure of the primary load path of the HSTA, which, in conjunction with a failure of the HSTA secondary nut, could result in loss of horizontal trim control and consequent reduced controllability of the airplane.

X

AD 2005-17-12 (Dye Pen Inspection) LH Wing

AD2005-17-12-1 051712-A This AD was prompted by reports of failed wing anti-ice ducts (piccolo tubes) in the leading edge of the wing. We are issuing this AD to prevent cracked piccolo tubes, which could result in air leakage, a possible adverse effect on the anti-ice air distribution pattern and anti-ice capability without annunciation to the flight crew, and consequent reduced controllability of the airplane

X

AD 2005-17-12 (Dye Pen Inspection) RH Wing

AD2005-17-12-2 051712-B This AD was prompted by reports of failed wing anti-ice ducts (piccolo tubes) in the leading edge of the wing. We are issuing this AD to prevent cracked piccolo tubes, which could result in air leakage, a possible adverse effect on the anti-ice air distribution pattern and anti-ice capability without annunciation to the flight crew, and consequent reduced controllability of the airplane

X




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AD 2005-17-12 (Terminating Action) LH Wing

AD051712-1 051712-1 This AD was prompted by reports of failed wing anti-ice ducts (piccolo tubes) in the leading edge of the wing. We are issuing this AD to prevent cracked piccolo tubes, which could result in air leakage, a possible adverse effect on the anti-ice air distribution pattern and anti-ice capability without annunciation to the flight crew, and consequent reduced controllability of the airplane

X

AD 2005-17-12 (Terminating Action) RH Wing

AD051712-2 051712-2 This AD was prompted by reports of failed wing anti-ice ducts (piccolo tubes) in the leading edge of the wing. We are issuing this AD to prevent cracked piccolo tubes, which could result in air leakage, a possible adverse effect on the anti-ice air distribution pattern and anti-ice capability without annunciation to the flight crew, and consequent reduced controllability of the airplane

X

AD 2005-18-06 000-12-160-701 051806A This AD was prompted by the development of terminating actions for the airplane flight manual (AFM) revisions. We are issuing this AD to prevent aileron control stiffness during flight, which could result in the reduction or possible loss of controllability of the airplane

X

AD 2005-18-06 000-27-590-722 000-27-690-722

051806B This AD was prompted by the development of terminating actions for the airplane flight manual (AFM) revisions. We are issuing this AD to prevent aileron control stiffness during flight, which could result in the reduction or possible loss of controllability of the airplane

X

AD 2005-18-06 000-12-590-702 000-12-690-702

051806C This AD was prompted by the development of terminating actions for the airplane flight manual (AFM) revisions. We are issuing this AD to prevent aileron control stiffness during flight, which could result in the reduction or possible loss of controllability of the airplane

X

AD 2005-18-06 000-12-160-700 051806D This AD was prompted by the development of terminating actions for the airplane flight manual (AFM) revisions. We are issuing this AD to prevent aileron control stiffness during flight, which could result in the reduction or possible loss of controllability of the airplane

X

AD 2005-23-01 000-53-280-607 052301A This AD results from a fatigue test which revealed cracking of the aft pressure bulkhead; subsequent in-service reports show that fatigue cracking has been found on certain other airplanes. We are issuing this AD to detect and correct cracking in the aft pressure bulkhead, which could result in reduced structural integrity and rapid decompression of the airplane.

X




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AD 2006-05-11 R1 AD2006-05-11B 060511B This AD results from a report that the shear pin located in the input lever of two pitch feel simulator (PFS) units failed due to fatigue. We are issuing this AD to prevent undetected failure of the shear pin of both PFS units simultaneously, which could result in loss of pitch feel forces and consequent reduced control of the airplane.

X

AD 2006-10-01 AD2006-10-01D 061001D To prevent fluid contamination inside the fire and overheat control unit in the flight compartment, which could result in a false fire alarm and consequent emergency landing.

X

AD 2006-10-01 (Terminationg Action)

AD2006-10-01E 061001E To prevent fluid contamination inside the fire and overheat control unit in the flight compartment, which could result in a false fire alarm and consequent emergency landing.

X

AD 2006-10-06 TBD AD061006 Relay Inspection and Replacement XAD 2006-11-09 AD2006-11-09 AD061109 This AD results from a report that a crack was

discovered at the lower forward corner of a cargo door skin cut-out during fatigue testing. We are issuing this AD to detect and correct cracking in the lower forward corner of the cargo door skin cut-out, which could result in reduced structural integrity of the airplane.

X

AD 2007-01-07 AD2007-01-07A-1 AD2007-01-07B-1

042009A1 This AD was prompted by a report of a cracked main fitting of the MLG. The FAA is issuing this AD to detect and correct fatigue cracking of the main fitting of the MLG and consequent failure of the main fitting, which could result in the collapse of the MLG

X

AD 2007-01-07 AD2007-01-07A-2 AD2007-01-07B-2

042009A2 This AD was prompted by a report of a cracked main fitting of the MLG. The FAA is issuing this AD to detect and correct fatigue cracking of the main fitting of the MLG and consequent failure of the main fitting, which could result in the collapse of the MLG

X

AD 2007-01-07 AD2007-01-07C-1 042009B1 This AD was prompted by a report of a cracked main fitting of the MLG. The FAA is issuing this AD to detect and correct fatigue cracking of the main fitting of the MLG and consequent failure of the main fitting, which could result in the collapse of the MLG

X

AD 2007-01-07 AD2007-01-07C-2 042009B2 This AD was prompted by a report of a cracked main fitting of the MLG. The FAA is issuing this AD to detect and correct fatigue cracking of the main fitting of the MLG and consequent failure of the main fitting, which could result in the collapse of the MLG

X


AD070107-1 AD070107 Terminating Action for AD 2007-01-07. Replacement of MLG main fittings P/N's: 17064-103 and -104.

X


AD070107-2 AD070107 Terminating Action for AD 2007-01-07. Replacement of MLG main fittings P/N's: 17064-103 and -104.

X




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AD 2007-03-19 AD2007-03-19A-1 041416A1 To detect and correct premature cracking of the main fittings of the MLGs, which could result in failure of the fittings and consequent collapse of the MLGs during landing

X

AD 2007-03-19 AD2007-03-19A-2 041416A2 To detect and correct premature cracking of the main fittings of the MLGs, which could result in failure of the fittings and consequent collapse of the MLGs during landing

X

AD 2007-03-19 AD2007-03-19B-1 041416B1 To detect and correct premature cracking of the main fittings of the MLGs, which could result in failure of the fittings and consequent collapse of the MLGs during landing

X

AD 2007-03-19 AD2007-03-19B-2 041416B2 To detect and correct premature cracking of the main fittings of the MLGs, which could result in failure of the fittings and consequent collapse of the MLGs during landing

X

AD 2007-04-24 AD070424A AD70424A CRJ Exhaust Tailcone Inspection XAD 2007-04-24 AD070424B AD70424B CRJ Exhaust Tailcone Bolt Replacement XAD 2007-07-07 AD0707-2 AD0707-2 Fan Disk Inspeciton XAD 2007-15-02 000-27-900-015 071502-A FNC (Backlash) Aileron Control System XAD 2007-15-02 000-27-900-150 071502-B FNC each Aileron PCU for INT Leakage XAD 2007-15-02 000-27-900-712 071502-C Backlash Chk and FNC Elevator Control System X

AD 2007-15-02 000-27-900-714 0715-02-D Backlash Chk and FNC Rudder Control System X

AD 74-08-09R2 AD74-08-09R2 To prevent possible fires that could result from smoking materials being dropped into lavatory paper or linen waste receptacles

X X X X X X X X X X

AD 2008-06-10 AD080610 AD080610 detect and correct cracking of the frame, whichcould lead to failure of the fuselage structure and possible loss of the airplane. X

AD 95-04-05 AD95-04-05 AD950405 To prevent the inability of passengers to exit the airplane in the event of an emergency X

C21-50-115-01 000-21-280-700 VCK Decompression Equalizer Rubber Diaphragm X

C24-10-129-01 000-24-900-701 B0520002 OPC GCU Overvoltage Protection XC24-20-129-01 000-24-220-701 B2423002 FNC (In-Flight Deployment) ADG XC24-20-129-01 000-24-900-702 B2423002 FNC (On Ground) Dry ADG XC25-17-152-01 000-25-220-701 FNC Cockpit Door Decompression Latch XC26-10-131-01 000-26-900-701 OPC APU Fire Diode XC26-20-131-01 000-49-310-120 GVI APU Firex Tubing XC26-20-131-02 LC2 OPC Eng, jetpipe, APU fire detection Sys XC26-20-131-03 LC2 Operational check of the APU Firex System XC27-10-105-01 000-27-900-001 OPC Aileron Disconnect System X X X X XC27-10-105-01 000-27-900-003 OPC Manual Roll Priority System X X X X XC27-10-105-03 000-27-900-720 FNC Aileron Breakout Bungee, Breakout Switch X

C27-10-105-05a 000-27-900-714 071502-D Backlash Check and FNC Rudder Control System X

C27-10-105-05b 000-27-900-712 071502-C Backlash Chk and FNC Elevator Control System X

C27-10-105-06 000-27-900-150 071502-B FNC each Aileron PCU for INT Leakage XC27-10-105-07 000-27-590-700 DVI LH Aileron Flutter Damper XC27-10-105-07 000-27-690-700 DVI RH Aileron Flutter Damper XC27-10-105-07 000-27-900-711 OPC AIL Flutter-Damp Fluid-level Xmtr Switch X




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CRJ 9648

CRJ 9672


C27-20-108-01 000-27-900-700 OPC Rudder Load Limiters XC27-30-102-01 000-27-900-706 OPC Pitch Disconnect System XC27-30-102-03 000-27-900-701 OPC Elevator Load Limiters XC27-30-102-05 000-27-330-100 DVI LH Elevator Flutter Dampers XC27-30-102-05 000-27-340-100 DVI RH Elevator Flutter Dampers XC27-30-102-05 000-27-900-108 OPC Elev Flutter-Damp Fluid-Level Xmtr-Sw XC27-31-102-01 000-27-220-003 FNC Pitch Feel Simulator Pilot Input Lever XC27-35-112-01 000-22-220-700 OPC Flight Control Panel (FCP) XC27-35-112-02 000-27-220-004 OPC Stall Protection (Flap Pos Transmitter) X X X X X X X X X XC27-40-103-01 Task Deleted per TR 2A-32.C27-40-113-01 LC2 Operational check of the Horiz Stab trim Sys XC27-42-103-01 000-27-320-102 DVI HSTA Secondary Load Path Indicator XC27-50-111-01 000-27-900-702 Backlash Check LH Wing Flap Actuators X X X X XC27-50-111-01 000-27-900-703 Backlash Check RH Wing Flap Actuators X X X X XC27-50-111-03 000-27-900-137 DVI LH Flap Actuator Ftgs, Trunnion Housing X X X X X X X X X XC27-50-111-03 000-27-900-138 DVI RH Flap Actuator Ftgs, Trunnion Housing X X X X X X X X X XC27-50-111-05 000-27-140-101 FNC Flap Electronic Control Unit XC27-50-111-06 000-27-580-701 B0520002 FNC LH Inbd Flap Actuator Torque Limiter XC27-50-111-06 000-27-590-742 B0520002 FNC LH Outbd Flap Actuator Torque Limiter XC27-50-111-06 000-27-680-701 B0520002 FNC RH Inbd Flap Actuator Torque Limiter XC27-50-111-06 000-27-690-742 B0520002 FNC RH Outbd Flap Actuator Torque Limiter XC27-50-111-07 000-27-580-002 DVI LH Wing Inboard Flap Actuator X X X X XC27-50-111-07 000-27-590-002 DVI LH Wing Outboard Flap Actuator X X X X XC27-50-111-07 000-27-680-002 DVI RH Wing Inboard Flap Actuator X X X X XC27-50-111-07 000-27-690-002 DVI RH Wing Outboard Flap Actuator X X X X XC27-50-111-08 000-27-900-007 OPC Skew Detection System (IBIT) X X X X X X X X X XC27-50-111-09 000-27-900-008 B2750001 FNC LH Wing Flap Actuator XC27-50-111-09 000-27-900-009 B2750002 FNC RH Wing Flap Actuator XC27-50-111-10 000-27-590-741 B2750003 FNC LH Outbd Flap Actuator Torque Limiter XC27-50-111-10 000-27-690-741 B2750004 FNC RH Outbd Flap Actuator Torque Limiter XC27-50-111-11 000-27-680-700 B2750005 FNC Inbd Flap Actuator Torque Limiter XC27-50-111-11 000-27-680-700 B2750005 FNC Inbd Flap Actuator Torque Limiter XC27-50-111-12 GVI visual portion of attachment inboard flap act

for condition and securityC27-50-300-01 000-27-580-007 B2750006 FNC Inbd Flap Actuator for Linear Endplay

(P/N: 601R93101-19) and (P/N: 852D100-19) X

C27-60-106-01 000-27-900-003 OPC Manual Roll Priority System X X X X XC28-00-142-01 LC2 OPC of the fuel crossflow XC28-20-131-01 000-28-900-702 Leak Test APU Fuel-Feed Shutoff Valve XC30-10-141-01 000-30-900-700 B0520002 FNC Wing A/I Overheat Sensors/Switches XC30-10-141-02 LC2 OPC Anti-Ice Duct sytem self-test XC31-40-158-01 000-31-220-700 OPC Data Concentrator Units XC34-10-141-01 000-34-220-723 FNC Altimeter Scale Error XC34-10-141-03 000-34-220-731 B3410001 FNC Altimeter Scale Error XC34-40-107-01 000-34-900-721 FNC Windshear Warning System XC35-10-128-01 000-35-900-702 VCK Crew Oxygen Bottle Pressure Gauge X X X X X X X X X XC36-20-133-01 000-36-220-700 OPC Bleed-Air Leak Detection System X X X X X X X X X XC36-20-133-02 000-36-220-700 OPC Bleed-Air Leak Detection System X X X X X X X X X XC52-10-821-01 000-52-830-700 B0520002 GVI Phase IV Pax Door Upper Latch Pins XCHQ-24-12-00-02 LC2 Service IDG's XCHQ-25-50-00-01 000-25-510-000 GVI of the Cargo Restraint Netting X X X X X X X X X XCHQ-38-11-01-07 CWATERSAMPLE B3811002 Potable Water Sampling Program XCR-25-62-02 CG25-60-00-212-001 GVI AED X X X X X X X X X XF12-20-00-01 LC1 Clean windshield & leading edges XR22-11-A083-01 000-12-160-701 LUB Aileron Servo Clutch XR27-00-A053-01 AD2005-18-06B 051806B DIS LH-Wing Outboard Aileron Pulleys X

P/N effective to this task does not exist on the CHQ fleet.




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CRJ 9672


R27-00-A053-01 AD2005-18-06B 051806B DIS RH-Wing Outboard Aileron Pulleys XR27-11-A082-01 000-12-590-702 LUB LH Wing airleron cables XR27-11-A082-01 000-12-690-702 LUB RH Wing airleron cables XR27-11-A082-02 000-12-160-700 LUB Aileron Aft Quadrant Trim Lever Bearings XR27-31-A024-01 Task Deleted per Rev. 7 Part 2 MRM.R27-50-300-01 000-27-590-740 B2750003 RST LH Wing Outboard Flap Actuators XR27-50-300-01 000-27-690-740 B2750004 RST RH Wing Outboard Flap Actuators XR32-31-828-01 000-32-220-700 DVI LG Control Handle Slider X X X X XR32-31-828-02 000-32-220-701 B3231001 RST LG Control Handle Assembly XR32-31-828-03 000-32-220-702 B3231002 RST LG Control Handle Assembly XR52-11-878-01 000-52-830-701 DVI Phase IV Pax Door Up Latch Ftgs Bush X X X X X X X X X XR72-21-802-01 LC1 VCK of the ENG Master Chip Detector Indicator X

REO 601R-32-10-008 NC

B3210001 DIS of the MLG Trailing Arm X

REO 601R-32-11-047 NC

B3211001 DIS of the MLG Main Ftgs Assembly X

REO 601R-32-11-161 NC

B3211002 DIS of the Main Landing Gear (MLG) Pivot Pin X

REO 601R-32-11-171 NC

B3211003 DIS of the Main Landing Gear (MLG) Pivot Pin X

REO 601R-32-11-182 NC

B3211004 DIS of the MLG Pintle Pin X

REO 601R-32-11-183 NC

B3211005 DIS of the MLG Pintle Pin X

REO 601R-32-21-109 NC

B3221002 DIS NLG Piston (Piston Tube) X

REO 601R-53-00-026 A B5300001 Generic Rpr-Cabin Window Surround Structure XREO 601R-53-00-030 C-a

B5300002 Generic Rpr-Fuse Skin Pax Door Up/Lwr Corner X

REO 601R-53-00-030 C-b

B5300003 Generic Rpr-Fuse Skin Pax Door Up Corner X

REO 601R-53-00-033 C-a

B5300004 Generic Rpr-Fuse Skin Svc Door Lwr Corners X

REO 601R-53-00-033 C-b1

B5300005 Generic Rpr-Fuse Skin Src Door Edges X

REO 601R-53-00-033 C-b2

B5300006 Generic Rpr-Fuse Skin Src Door Edges X

REO 601R-53-00-034 D B5300007 Generic Rpr-Fuse Skin Non-Flush Cargo pit XREO 601R-53-00-061 A Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-11-006 NC, A, B, C

B5311001 Repair to Fuse Skin, FS 235.00 X

REO 601R-53-11-010 NC, A, B, C

B5311002 Repair to Fuse Skin, FS 235.00 X

REO 601R-53-11-048 A B5311003 Repair to Fuse Skin Radius, FS 235.00 XREO 601R-53-11-162 NC

Task Deleted per Rev. 7 Part 2 MRM.

REO 601R-53-11-276 NC-1

B5311005 Repair to Bulkhead Channel X

REO 601R-53-11-276 NC-2

B5311006 Repair to Bulkhead Channel X

REO 601R-53-21-180 NC-1


REO 601R-53-21-180 NC-2





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REO 601R-53-21-183 NC-1


REO 601R-53-21-183 NC-2


REO 601R-53-21-313 NC-1


REO 601R-53-21-313 NC-2


REO 601R-53-31-012 C or D-1


REO 601R-53-31-012 C or D-2


REO 601R-53-31-019 NC to C


REO 601R-53-41-010 NC


REO 601R-53-41-057 NC


REO 601R-53-41-067 NC


REO 601R-53-41-102 NC


REO 601R-53-41-103 A Task Deleted per Rev. 7 Part 2 MRM.REO 601R-53-61-1240 NC-1

B5361001 Repair & Mod Press Bulkhead Web X

REO 601R-53-61-1240 NC-2

B5361002 Repair & Mod Press Bulkhead Web X

REO 601R-53-61-1285 NC-1

B5361003 Repair to FS 621.00 Pressure Bulkhead Web X

REO 601R-53-61-1285 NC-2

B5361004 Repair to FS 621.00 Pressure Bulkhead Web X

REO 601R-53-61-345 D-a

A5361005 Generic Rpr-Eng Support Beam Up/Lwr Webs, LH X

REO 601R-53-61-345 D-a

B5361005 Generic Rpr-Eng Support Beam Up/Lwr Webs, RH X

REO 601R-53-61-345 D-b

A5361006 Generic Rpr-Eng Support Beam Up & Lwr Webs, LH X

REO 601R-53-61-345 D-b

B5361006 Generic Rpr-Eng Support Beam Up & Lwr Webs, RH X

REO 601R-53-61-358 A A5361007 Repair to Eng Support Beam Lwr Web, LH XREO 601R-53-61-358 A B5361007 Repair to Eng Support Beam Lwr Web, RH XREO 601R-53-61-366 E-a

B5361008 Repair-Eng Support Beam Lwr Web X

REO 601R-53-61-366 E-b

A5361009 Repair to Eng Support Beam Lwr Web X

REO 601R-53-61-366 E-b

B5361009 Repair to Eng Support Beam Lwr Web X

REO 601R-53-61-368 NC

B5361010 Deviation to REO 601R-53-61-345 X

REO 601R-53-61-530 NC

B5361011 Deviation to REO 601R-53-61-345, Upper Web X

REO 601R-53-61-531 NC

B5361012 Deviation to REO 601R-53-61-345, Lwr Web X

REO 601R-53-61-870 B B5361013 Repair to ENG Support Beam Upper & Lwr Webs X




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CRJ C5

CRJ 24

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CRJ 72

CRJ 7248

CRJ 9648

CRJ 9672


REO 601R-55-11-061 NC-a


REO 601R-55-11-061 NC-b


REO 601R-55-21-080 NC-a


REO 601R-55-21-080 NC-b


REO 601R-55-21-082 NC-a


REO 601R-55-21-082 NC-b


REO 601R-57-21-037 NC

B5721001 Instal Ovrsize Bushing Wing-Fuse PickUp Ftgs X

REO 601R-57-21-046 NC

B5721002 Int Repair-Aft Lwr Wing Plank X

REO 601R-57-21-130 C B5721003 Repair to Lwr Wing Plank WS 148.019, LH & RH X

REO 601R-57-21-131 NC


REO 601R-57-21-169 NC

B5721005 Rpr-Aft Wing Plank Fuel Pump-Satellite Hole X

REO 601R-57-61-004 B B5761005 Repair-Oversize Bushings - Aileron Ctr Hinge XREO 601R-57-61-052 NC

B5761006 Repair to Aileron PCU Ftgs Lugs X

REO 601R-53-61-358 A B5361007 Repair to Eng Support Beam Lwr Web, RH XREO 601R-53-61-366 E-a

B5361008 Repair-Eng Support Beam Lwr Web X

REO 601R-53-61-366 E-b

A5361009 Repair to Eng Support Beam Lwr Web X

REO 601R-53-61-366 E-b

B5361009 Repair to Eng Support Beam Lwr Web X

REO 601R-53-61-368 NC


REO 601R-53-61-530 NC

B5361011 Deviation to REO 601R-53-61-345, Upper Web X

REO 601R-53-61-531 NC

B5361012 Deviation to REO 601R-53-61-345, Lwr Web X

REO 601R-53-61-870 B B5361013 Repair to ENG Support Beam Upper & Lwr Webs X

REO 601R-55-11-061 NC-a

B5511001 Repair-Horiz Stab Elevator Hinge Ftgs X

REO 601R-55-11-061 NC-b

B5511002 Repair-Horiz Stab Elevator Hinge Ftgs X

REO 601R-55-21-080 NC-a

B5521001 Repair-Elevator Hinge Ftgs X

REO 601R-55-21-080 NC-b


REO 601R-55-21-082 NC-a


REO 601R-55-21-082 NC-b


REO 601R-57-21-030 NC A, B, C, D

SDI Wing Lower Plank Access Holes

REO 601R-57-21-037 NC


Task accomplished via AWL's: 57-21-146, 57-21-147, 57-21-148, 57-21-149.




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CRJ 24

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CRJ 7248

CRJ 9648

CRJ 9672


REO 601R-57-21-046 NC


REO 601R-57-21-130 C B5721003 Repair to Lwr Wing Plank WS 148.019, LH & RH X

REO 601R-57-21-131 NC


REO 601R-57-21-169 NC


REO 601R-57-61-004 B Task Deleted per Rev. 7 Part 2 MRM.REO 601R-57-61-052 NC



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