78-10-03[1]

Fokker Services B.V. Nieuw-Vennep

The Netherlands All rights reserved by Fokker Services B.V.,(The Netherlands). This document has been supplied by Fokker Services B.V. to its customer on a confidential basis subject to the provisions of an agreement. Reproduction or disclosure to third parties of this document or any part thereof, or the use of any information contained therein for purposes other than explicitly allowed by the aforesaid agreement, is not permitted except with the prior written permission of Fokker Services B.V..

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ABBREVIATED COMPONENT MAINTENANCE MANUAL

WITH ILLUSTRATED PARTS LIST

JET PIPE ASSEMBLY

PART NUMBERS

F1107-452-401 F1107-452-408 F1107-452-402 F1107-452-411 F1107-452-403 F1107-452-412 F1107-452-407

PREVIOUS ISSUE DATE: JUL 01/95 REVISION DATE: SEP 01/01

COMPONENT MAINTENANCE MANUAL P/N F1107-452

TRANSMITTAL LETTER 78-10-03 Page 1/2SEP 01/05

TRANSMITTAL LETTER FOR ACMM 78-10-03

UNIT TITLE : Jet Pipe Assembly : F1107-452-401 REVISION NUMBER : 004PART NUMBER F1107-452-402 REVISION DATE : SEP 01/05

F1107-452-403 PREVIOUS REVISION DATE : SEP 01/01 F1107-452-407 F1107-452-408 F1107-452-411 F1107-452-412

This is a revision of the Abbreviated CMM 78-10-03. It consists of 15 pages, including the title page. The ACMM does not contain a list of effective pages, because if a revision is necessary, it will be re-issued as a whole. Problems, comments and requests for change or improvement to this manual must be addressed to:

Fokker Services BV Technical Services/Maintenance & Documentation P.O. Box 231 2150 AE NIEUW-VENNEP The Netherlands Telephone : +31 (0) 252 627350 Fax : +31 (0) 252 627211 E-mail : [email protected]

"END"


HIGHLIGHTS 78-10-03 Page 1/2SEP 01/05

HIGHLIGHTS FOR ACMM 78-10-03

UNIT TITLE : Jet Pipe Assembly : F1107-452-401 REVISION NUMBER : 004PART NUMBER F1107-452-402 REVISION DATE : SEP 01/05

F1107-452-403 F1107-452-407 F1107-452-408 F1107-452-411 F1107-452-412

This issue reflects data corrections on the pages 1, 2, 5, 7, 8, 9, 10 and 11.

The following list details the pages affected by this revision and the reasons for their change: SUBJECT PAGE REASON FOR CHANGE Title Page 1 Footer up-dated. Technical Contents 2 Revision data up-dated.

5 Typo error in Note 6 corrected. 7 Typo error in Note 1 corrected. 8 MIL reference in paragraph 8C(2) corrected. 9 Item 5 in table 4 added. 10 Material number item 6 in table 5

corrected and the Brush, Stiff Bristle transferred to table 4.

11 Vendor code H0W98 added and textual corrections made.

END

COMPONENT MAINTENANCE MANUALP/N F1107-452


UNIT TITLEPART NUMBER REVISION NUMBER

REVISION DATEPREVIOUS REVISION DATE

003SEP 01/01JUL 01/95

Jet Pipe AssemblyF1107-452-401F1107-452-402F1107-452-403F1107-452-407F1107-452-408F1107-452-411F1107-452-412

This is a revision of the Abbreviated CMM 78-10-03. It consists of 15 pages,including the title page. The ACMM does not contain a list of effective pages,because if a revision is necessary, it will be re-issued as a whole.

Problems, comments and requests for change or improvement to this manual mustbe addressed to:

Fokker Services BVTechnical Services/Maintenance & DocumentationP.O. Box 2312150 AE NIEUW-VENNEPThe Netherlands

Telephone : +31 (0) 252 627350Fax : +31 (0) 252 627211E-mail : [email protected]

"END"

TRANSMITTAL LETTER 78-10-03 Page 1/2SEP 01/01



UNIT TITLE : Jet Pipe AssemblyPART NUMBER : F1107-452-401 REVISION NUMBER : 003

F1107-452-402 REVISION DATE : SEP 01/01F1107-452-403F1107-452-407F1107-452-408F1107-452-411F1107-452-412

This issue reflects data corrections in the repair chapter 7.

The following list details the pages affected by this revision and the reasonsfor their change:

SUBJECT PAGE REASON FOR CHANGE

Title Page 1 To show the new company logo.

Technical Contents 5 Crack sizes in Note 4 corrected.7 Small crack size in table 3

corrected.

'END"

HIGHLIGHTS 78-10-03 Page 1/2SEP 01/01

Daimler-BenzAerospace



UNIT TITLE : Jet Pipe AssemblyPART NUMBER : Fl107-452-401 REVISION NUMBER : 002

F1107-452-402 REVISION DATE : JUL 01/95F1107-452-403F1107-452-407Fl107-452-408F1107-452-411F1107-452-412

This revision incorporates a jet pipe repair.The following list details the pages affected by this revisions and the reason forchange:

SUBJECT PAGE REASON FOR CHANGE

Title Page 1 Re-issued for ACMM

Technical Content 2 thru 5 Revised description of jet pipe6 and 7 Incorporated Table 2 Forward Jet Pipe

Repair and Table 3 Rear Jet Pipe Repair

8 thru 11 Re-issued for ACMM

12 thru 14 Revised illustration and nomenclature.

"END"

HIGHLIGHTS 78-10-03


2409f


UNIT TITLEPART NUMBERS REVISION NUMBER


001JAN 01/94JAN 01/91


This revision corrects technical detail contained in the manual, adds new assemblyversions -411/-412 and re-issues the CMM as an ACMM.

The following list details the pages affected by this revision and the reasons fortheir change.

SUBJECT

Title Page

PAGE

1

REASON FOR CHANGE

Cover re-issued for ACMM. Assemblyversions added

Record of Revisions

Record of Temporary Revisions 1/2

Service Bulletin List

List of Effective Pages

Table of Contents

Introduction

Technical Content

1/2

1/2

1/2

1/2

1 and 2

1/2

2 thru 8

Deleted

Deleted

Deleted

Deleted

Deleted

Deleted

Present

Illustrated Parts List 9 thru13

Presentation of information changedto reflect ACMM format. Revisionrecord added. Para 1.A. assemblyversions added. Figure 2 and Repairprocedures revised to reflect updatedmaintenance procedures. Radiological(X-ray) inspection procedure deleted.Ultrasonic crack test proceduredeleted. Tables 2 and 3 revised toreflect updated maintenance proc-eduresIntroduction of Illustrated Parts List.

"END"

HIGHLIGHTS 78-10-03 Page 1JAN 01/94


Daimler-BenzAerospace


UNIT TITLEPART NUMBER REVISION NUMBER


002JUL 01/95JAN 01/94

: Jet Pipe Assembly: F1107-452-401F1107-452-402Fl107-452-403F1107-452-407F1107-452-408F1107-452-411F1107-452-412

This is a revision of ACMM 78-10-03. The List of Effective Pages is the onlydocument to be used for checking your manual for correct contents.Problems, comments and requests for change or improvement to this manual must besent to the Fokker Technical Support Department at the following address:

Fokker Aircraft B.V.Technical Support Turboprop AircraftP.O. Box 122221100 AE AMSTERDAM ZUID-OOSTThe Netherlands

Telephone :Fax :Telex :Sita :

+31 20 6057301+31 20 605755511526 fmhs nlamsfk7x

'END"

TRANSMITTAL LETTER 78-10-03 Page 1JUL 01/95


2409f


UNIT TITLEPART NUMBERS REVISION NUMBER


001JAN 01/94JAN 01/91


This is a re-issue of ACMM 78-10-03. The re-issued manual consists of thirteenpages which includes the cover.

Remove and destroy all the existing pages and replace them with the contents ofthis revision.

Problems, comments and requests for change or improvement to this manual must beaddressed to the Fokker Technical Publications Department at the followingaddress:

Fokker Aircraft B.V.Technical Publications DepartmentP.O. Box 122221100 AE AMSTERDAM ZUID-OOSTThe Netherlands

Telephone:Fax:Telex:Sita:

(31) 20 6057501(31) 20 605755511526 fmhs nlamsfkcr

"END1

TRANSMITTAL LETTER 78-10-03 Page 1JAN 01/94


2409f

TRANSITITTAL LETTER FOR CMM 78-10-03

UNIT TITLE-PART NUMBERS REVISION NUMBER


000JAN 01/91

Jet Pipe AssemblyF1107-452-401F1107-452-402F1107-452-403F1107-452-407F1107-452-408

This is your first issue of CMM 78-10-03. The List of effective pages is theonly document to be used for checking your manual for correct contents.

Problems, comments and requests for change or improvement to this manual mustbe to the Fokker technical publications department at the following address:

Technical Publications DepartmentFokker Aircraft BVPO Box 122221100 AE AMSTERDAM-ZOThe Netherlands

"END1

TRANSMITTAL LETTER 78-10-03 Page 1/2JAN 01/91


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Rev. No. 000 001 002 003 004

Date of Issue

JAN 01/91 JAN 01/94 JAN 01/95 SEP 01/01 SEP 01/05

1. Description and Operation

A. General

The jet pipe attaches the engine jet pipe and is produced in seven versions, the assemblies 401, -402, -403, -407, -408, -411 and 412. Equipment specifications of the jet pipe are given below:

CHARACTERISTICS SPECIFICATIONS

Length Width Height

521 mm (20.5 in)

Equipment Specifications

Table 1

B. Physical Description (Refer to Figure 1) The jet pipe is produced in two sections, the forward section and the rear section. The forward section is fitted with a bell end and a female flange. The bell end attaches the jet pipe to the nacelle structure. The female flange is fitted to the lower end of the forward jet pipe. The rear jet pipe is fitted with a male flange and two outer rings. The male flange abuts the female flange joining the forward and rear jet pipe. The rear jet pipe is fitted with a strip and two outer rings. These outer rings provide a support for securing the jet pipe in the engine nacelle. The strip is spot-welded to the end of the rear jet pipe.

C. Functional Description The jet pipe has been designed to direct the engine exhaust gases clear of the engine nacelle.

D. Theory of Operation (Not Applicable

2. Testing and Fault Isolation (Not Applicable)

3. Automatic Testing and Fault Isolation (Not Applicable)


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COMPONENT MAINTENANCE MANUAL P/N A83235

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MATERIAL P/N PROD. INC A/C S/N/SB

TYPICAL DAMAGE REPAIRS AND LIMITATIONS

CPM-TH5.141 AISI 321

F1107-452 -401,-402, -701, -702

20103

1. Spider web cracks and (large) holes caused by carburising of material 2. Cracks at spot welded aft- strip 3. Cracks near spot-welded outer rings < 200 mm (one crack), total length of cracks < 300 mm (multiple cracks)4. Cracks exceeding 3 5. Small cracks < 20 mm

1. No repair possible 2. Replace spot-welded aft strip (partly) by welded (5.150) aft- strip with double thickness 3. Welded patch repair (maximum 2 patches allowed) 4. No repair possible 5. Weld repair

CPM-TH5.150 Nitronic 40

F1107-452 -407, -408, -703, -704

20173 SBF50-78 -002

1, Cracks near spot-welded outer rings < 200 mm (one crack), total length of cracks < 300 mm (multiple cracks)4. Cracks exceeding 1 5. Small cracks < 20 mm

1. Welded patch repair (maximum 2 patches allowed) 2. BPS 209 repair (rebuilt) * 3. Weld repair

CPM-TH5.150 Nitronic 40

F1107-452 -411, -412, -707, -708

20267 1. Cracks near seam welded outer rings < 200 mm (one crack), total length of cracks < 300 mm (multiple cracks)2. Cracks exceeding 1 3. Small cracks < 20 mm

1. Welded patch repair (maximum 2 patches allowed) 2. BPS 209 repair (rebuilt) * 3. Weld repair

NOTES: 1. All welding repairs: TIG welding with Hastelloy W (nickel). 2. (*) These repairs must be sent to Fokker Material Support for BPS 209 repair. 3. The 700 type assemblies have pre-drilled holes in their outer rings for spare delivery.

Rear Jet Pipe Repair

Table 3


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8. Assembly and Storage

A. Materials Refer to table 5.

B. Assembly Procedures (Not Applicable)

C. Storage

CAUTION: DO NOT STORE THE UNIT IN THE VICINITY OF CORROSIVE FLUIDS OR NEAR HEAT- OR OZONE GENERATING SOURCES.

(1) General

(a) The storage area must be clean and well ventilated. (b) The temperature of this area must be between minus 20C and plus

70C (-4F and +158F). (c) The air in the area shall have a relative humidity of 65%

maximum. (d) Put the packed unit in such a position, that it is easy to read

the identification label.

(2) Preservation

Do the preservation procedure (refer to the MIL-STD-2073-1 specification).

(3) Packing

(a) Prepare two identification labels.

Make sure that the identification label shows: 1 The part or type number of the unit. 2 The serial number of the unit. 3 The date of last inspection or test of the unit. 4 The initial date of storage.

(b) Attach one of the identification labels to the unit. (c) Put quantities of desiccant (Fk15-010) in some cotton bags. (d) Put the unit, together with the cotton bags into the original

packing or in a suitable container (Refer to the ATA 300 specification).

(e) Attach the remaining identification label to the outside of the container.

NOTE: If the identification label is missing, the unit cannot be approved for storage or installation.

9. Fits and Clearances (Not Applicable)


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10. Special Tools, Fixtures, Equipment and Materials

A. General This paragraph contains the special tools, equipment and materials required to perform the procedures detailed in this manual.

B. Special Tools and Equipment The following table lists the special tools and equipment required to perform all the procedures detailed in this manual.

Equivalent substitutes may be used for the listed items.

ITEM NO.

NOMENCLATURE SPECIFICATION/PART NUMBER

QTY VENDOR CODE

UTILIZATION

TESTING

DISASSY

CLEANING

CHECK

REPAIR

ASSY/STORE

1 Air Source, Adjustable 0-193 kPa

(0-28 psi) 1 Local X

2 Drill 2,5 mm (3/32 in)

1 Local X

3 Equipment, Dye Penetrant Crack Detection

1 Local X

4 Equipment, Welding, Tungsten Inert Gas (TIG)

1 Local X

5 Brush, Stiff Bristle 1 Local X

Special Tools and Equipment

Table 4

C. Materials The following table lists the materials required to perform all the procedures detailed in this manual. For further details refer to the Consumable Materials List.

Equivalent substitutes may be used for the listed items.


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ITEM NO.

NOMENCLATURE MATERIAL NUMBER

VENDOR CODE

UTILIZATION

TESTING

DISASSY

CLEANING

CHECK

REPAIR

ASSY/STORE

1 Cloth, Cleaning (Lint Free Cloth) Fk05-044 Local X 2 Alcohol, Acetone Fk11-001 Local X3 Solvent, Methyl Ethyl Ketone (MEK) Fk11-003 Local X4 Solvent Cleaning, (White Spirit) Fk11-007 Local X 5 Desiccant, Dehumidification Fk15-010 Local X6 Welding Material, Hastelloy-W AMS5786

P/N FRF01311-78045

H0W98 X

Materials Table 5

11. Illustrated Parts List

A. Introduction

(1) Purpose The purpose of this illustrated parts list is to provide a means of locating and identifying parts of the unit and to facilitate the provisioning, storing and issuing of replaceable parts, in accordance with the approved shop maintenance policy.

(2) How to use the IPL Illustrations are provided on which the replaceable items in the unit are shown. These illustrations identify the parts by means of item numbers. The physical location and the item number of each part are thus determined by examination of the appropriate illustration. Each illustration is followed by a detailed parts list in which all the parts are listed in item number sequence. From this list the user can obtain the part number, description, usage and quantity of each item.


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The nomenclature is indented to show the relationship to the main assembly. A dash (-) in the Fig. Item column, preceding the number, indicates that the item is not shown on the illustration.

The effectivity codes column gives a letter to each main assembly in

an IPL figure. The same letter then denotes items, which can be used with all non-coded items in the main assembly. Where applicable, vendors are identified by a code number, preceded by a capital V, following the item description in the nomenclature column. The code number is as given in the last issue of the H4/H8 Commercial Activity/Government Entity) (CAGE) data box. The CAGE is also known as the Federal Supply Codes For Manufacturers (FSCM). For detailed information concerning F0N numbers refer to the Standards Manual Substitute and Equivalent List, Technical Handbook (TH)-16.

B. Effectivity Codes

The following effectivity codes have been assigned to this manual:

EFFECTIVITY CODE

PART NUMBER ASSEMBLY

FIGURE

A F1107-452-401 IPL 1 B F1107-452-407 IPL 1 C F1107-452-411 IPL 1 A F1107-452-402 IPL 2 B F1107-452-408 IPL 2 C F1107-452-412 IPL 2 A F1107-452-403 IPL 3

C. Vendor Codes, Names and Addresses

VENDOR CODE

VENDORS NAME AND ADDRESS

H0W98

Fokker Services BV. Material Support Lucas Bolsstraat 7 2152 CZ NIEUW-VENNEP The Netherlands


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Return to CMM Index

78-10-03[1]

Documents

number f1107

numbers f1107

revision data

change title page

fokker services bvtechni

list of effective pages

subject page reason

manual mustbe