yte lh 722283...cfm56-3, 3b, 3c to prevent agb starter gearshaft failure,which could result in ifsd...

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Page 1: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the
Page 2: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the
Page 3: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the
Page 4: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the
Page 5: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the
Page 6: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

AS TO DATE : January 31, 2013ENGINE MODEL : CFM56-3C-1 TOTAL ENGINE TIME : 60137.57SERIAL NUMBER : 722283 TOTAL ENGINE CYCLES : 39308

SB REFERENCE ISSUENUMBER EFFECT. DATE HOURS CYCLES

1 86-08-05 R1 72-205 R5 7-Jul-86 CFM56-3/3BINSPECTION OF RDS OIL DISTRIBUTOR P/N:335-305-800-0-1 AND SPIROLOCK P/N:649-363-137-0

N/A

SB Torque check increases from 50 inch-lbs to 100 inch- lbs is required prior to inspection for the pupose of this AD

N/A to TGB PN installed. Ref. UAL AD Compliance Records on 17 Dec 2008.

2 89-13-51 737-71-1203 29-Jan-97FAN DISK PN:335-04-511-0 & FAN BLADES PNs: 9527M99P08P09& 1285M39P01 REMOVAL.(OPERATED AT RESTRICTED CFM56-3C-1 THRUST)

S SUPERSEDED SUPERSEDED BY AD 96-25-11

3 89-17-04 28-Jan-98

INSPECT FORWARD SUMP MCD AND REMOVED THE AFFECTED NO.3 BEARING PN:9732M10P12 SNs FAFDxxxx or FAFExxxx) PN: 9732M10P18, or 1376M76P12 FROM SERVICE

S SUPERSEDED SUPERSEDED BY AD 89-23-06 R1

NO 3 BEARING MCD INSPECTION MCD INSPECTION

Inspect MCD within the next 50 hrs TIS after the EOD of this AD. E-inspect at interval not to

d 50 h TIS i l t No.3 Bearing PN installed not

APPLICABILITY NEXT DUE REMAIN METHOD OF COMPLIANCESTATUS INTERVALLAST ACCOMPLISHED

AIRWORTHINESS DIRECTIVE COMPLIANCE STATUSENGINE

FAA AD NO.NO DESCRIPTION REMARKS

4 89-23-06 R1 72-530 R3 28-Jan-98 CFM56-2,3,3B, 3C & -5

NO.3 BEARING MCD INSPECTION MCD INSPECTION PROGRAM REPLACEMENT OF NO.3 OR INSPECTION OF MCD ACC. TO P/N AND S/N

N/Aexceed 50 hrs TIS since last inspection or remove the NO.3 bearing PN: 9732M10P18 & PN: 1362M76P02 from service at the next shop visit or before 31 Jan 1998 whichever come first.

o 3 ea g sta ed otaffected.Ref. UAL AD Compliance Records on 17 Dec 2008.

90-15-14 737-26-2055 23-Aug-90

737-300/400 EQUIPPED

WITH KIDDIE ENGINE FIRE

AND OVERHEAT DETECTION SYSTEMS.

TO REDUCE FALSE ENGINE FIRE AND OVERHEAT WARNINGS, EHICH COULD RESULT IN UNNECESSARY ENGINE IN-FLIGHT SHUTDOWNS AND AIRPLANE DIVERSION THAT UNDULY JEOPARDIZE CONTINUED SAFE OPERATION OF THE AIRPLANE.

I/P 30-Apr-07

Modify the engine fire and overheat detection system on each engine in accordance with Boeing Service Bulletin 737-26-1055, revision 1 dated September 14, 1989.

Found Incorporated Previously. Ref. UAL AD Compliance Records on 17 Dec 2008.

5 90-20-13 72-494 R2 14-Oct-90 CFM56-3B, -3C

TO PREVENT FAN BLADE FAILURE, IFSD, AND SEVERE ENGINE DAMAGE BY INCORPORATING THE FAN BLADE DAMPERS PN: 335-105-305-0, AXIAL STOPS PN: 335-105-201-0, AND BOLTS PN: J815P056A, TO THE FAN MODULE ASSEMBLY.

T 16-Oct-90

Modify the fan module by installing the fan blade dampers, axial stops and bolts within 60 days from the EOD of this AD. (EOD: 14 Oct 1990)

Found Incorporated Previously. Perform in accordance with SB CFM56-72-494.Ref. UAL AD Compliance Records on 17 Dec 2008.

6 91-02-10 72-450 R1 11-Feb-91 CFM56-3, 3B, 3C

INSTALLATION OF NEW SPLITTER FAIRING, STAGE 1 VANE ASSY, & NEW CENTERING SHROUD T 22-Nov-89

If a later revision of the Service Bulletin is used for complying with this FAA-AD recorded

Incorporated Previously. Perform in accordance with SB 72-450 R1. Ref. UAL AD Compliance Records on 17 Dec 2008.

7 91-02-10 72-462 R1 11-Feb-91 CFM56-3, 3B, 3C

INSTALL THE 12 DOOR VARIABLE BYPASS VALVE (VBV) CONFIGURATION T 15-Nov-89

If a later revision of the Service Bulletin is used for complying with this FAA-AD recorded

Incorporated Previously. Perform in accordance with SB 72-462 R1. Ref. UAL AD Compliance Records on 17 Dec 2008.

Page 7: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

AS TO DATE : January 31, 2013ENGINE MODEL : CFM56-3C-1 TOTAL ENGINE TIME : 60137.57SERIAL NUMBER : 722283 TOTAL ENGINE CYCLES : 39308

SB REFERENCE ISSUENUMBER EFFECT. DATE HOURS CYCLES

APPLICABILITY NEXT DUE REMAIN METHOD OF COMPLIANCESTATUS INTERVALLAST ACCOMPLISHED

AIRWORTHINESS DIRECTIVE COMPLIANCE STATUSENGINE

FAA AD NO.NO DESCRIPTION REMARKS

8 96-18-16 72-695 9-Dec-96CFM56-2, 2A,

2B, 3, 3B, 3C & 5

TO PREVENT LCF FAILURE OF LPT ROTOR (LPTR) STUB SHAFT AND CONICAL SUPPORT, WHICH COULD RESULT IN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

N/A

For CFM56-3,-3B,-3C, reidentify the LPTR stub shaft, PN: 301-330-618-0/619-0/623-0/624-0, with S/N listed in Table 2 of SB72-695. To be carried out at next piece-part exposure after the EOD of this AD but not to exceed a total thrust rating life cycles of 20,000 (Cat.A)/11.400 (Cat.B)/7,900 (Cat.C). (EOD: 29 Jan 1997)

N/A to Both Conical Support & Stub shaft PN: Installed.Ref. UAL AD Compliance Records on 17 Dec 2008.

9 96-25-11 72-543 R4 29-Jan-97 CFM56 3B2, 3C1

TO PREVENT FAN BLADE FAILURE BY REMOVING AFFECTED FAN DISK & BALDE SET OPERATED AT UNRESTRICTID CFM56-3C-1 THRUST LEVELS.

N/A

Fan Disk have not operated at unrestricted CFM56-3C-1Thrust Levels

N/A. Ref. UAL AD Compliance Records on 17 Dec 2008.

10 97-08-01 Engine Shop Manual Chapter 5 23-Jun-97 CFM56-3, -3B,

3C

TO PREVENT A LACF FAILURE OF THE FAN DISK, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE

N/ANew Cat-C thrust rating LCF retirement life of 20,100 cys introduced

P/N installed found affected by this AD but the current fan disk CAT A thrust rating life is 30000 cycles, and is not affected by this AD. SEE LLP SUMARY FOR LIFE REMAINING. Ref. UAL AD Compliance Records on 17 Dec 2008.

11 T97-25-51 3-Jun-98 CFM56-3, -3B, 3C

TO PREVENT IFSD DUE TO AN AGB STARTER GEARSHAFT OR TGB INPUT BEVEL GEAR FAILURE S SUPERSEDED SUPERSEDED BY AD 98-10-11

12 98-07-02 SB 72-856 SB 72-855 30-Mar-98 CFM56-2,3,3B,

3C

TO PREVENT RUBS BETWEEN TH E OUTER CONE OF THE NO.3 BEARING AFT. STA. AIRSEAL AND STAGE 1-2 HPC SPOOL, WHICH COULD RESULT IN A POTENTIAL UNCONTAINED ENGINE FAILURE.

N/A

Install no.3 Bearing Aft. A/O Seal retention bushings per SB72-855 and/or remove the Stage 1-2 HPC spool PN: 1589M66P02 with a list of affected S/Ns at the next shop visit that 1st confirmed the rub event or whichever come first.

No.3 Bearing aft stationary A/O seal PN found not affected by this AD. And HPC 1-2 spoll SN found not affected by this AD. Ref. UAL AD Compliance Records on 17 Dec 2008.

13 98-10-11

SB 72-A861R3 SB 72-863R1R1

SB 72-865 SB 72-867

SB 72-873R1

3-Jun-98 CFM56-3, 3B,3C,5,5B,5C

TO PREVENT IFSD DUE TO AGB STARTER GEARSHIFT, TGB INPUT BEVEL GEAR, TGB OUTPUT BEVEL GEAR, AGB GEARSHAFT CLUSTER SPUR ASSY OR AGB INTERMEDIATE GEAR ASSY FAILURE.

N/A

Check the MCD prior to further flight and/or replace the affected parts/assemblies to serviceable parts per related SB72-861/863/865/867/873.

AGB and TGB PN found not affected by this AD.Ref. UAL AD Compliance Records on 17 Dec 2008.

14 98-12-32 SB 72-843 R1 20-Jul-98 CFM56-2, 2A, 2B, 3, 3B, 3C

TO PREVENT THE POTENTIAL FOR AN UNCONTAINED FAILURE OF THE HPT ROTOR DISK, WHICH COULD RESUKT IN AN IFSD, ATO OR DAMAGE TO AIRCRAFT.

N/A ECI for cracks/gouges in HPTR Disk.

HPT Disk PN Found Not affected by this AD.Ref. UAL AD Compliance Records on 17 Dec 2008.

15 98-19-10 SB 72-877 R1 28-Sep-98 CFM56-3, 3B, 3C

TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING.

N/AReplace suspected gearshaft within 350 hrs TIS after the EOD of this AD (EOD: 28 Sept 1998)

ESN 722283 and its installed AGB were both not affected by this AD and/or SB72-877R1.Ref. UAL AD Compliance Records on 17 Dec 2008.

Page 8: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

AS TO DATE : January 31, 2013ENGINE MODEL : CFM56-3C-1 TOTAL ENGINE TIME : 60137.57SERIAL NUMBER : 722283 TOTAL ENGINE CYCLES : 39308

SB REFERENCE ISSUENUMBER EFFECT. DATE HOURS CYCLES

APPLICABILITY NEXT DUE REMAIN METHOD OF COMPLIANCESTATUS INTERVALLAST ACCOMPLISHED

AIRWORTHINESS DIRECTIVE COMPLIANCE STATUSENGINE

FAA AD NO.NO DESCRIPTION REMARKS

16 2000-05-22 SB 72-922 2-May-00CFM56 -2, 2A,2B, 3, 3B, 3C TO DETECT CRACKS IN THE BOLT HOLES OD HPT

FRONT ROTATING AIR SEALS PN: 1282M72P03 N/A

Perform one time ECI to the listed HPT rotating airseals SNs per SB72-922 and based upon engine model and thrust ratings. (EOD: 2 May 2000)

N/A to HPT Front Rotating Airseals PN INSTALLED.Ref. UAL AD Compliance Records on 17 Dec 2008.

17 2000-12-01 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

TO PREVENT CRITICAL LIFE LIMITED ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN UNCONTAINED ENGINE FAILURE AND DAMAGAE TO THE AIRLPANE

S SUPERSEDED SUPERSEDED BY AD 2002-13-03

18 2000-15-0173-126 R1 73-125 R1 2-Oct-00

CFM56 -2, 2A,2B, 3, 3B, 3C,5 5A 5B 5C

TO PREVENT FUEL LEAKAGE FROM BETWEEN THE FUEL PUMP FILTER COVER AND GEAR HOUSING WHICH COULD RESULT IN AN ENGINE FIRE AND T 5-Sep-03

Perform initial/repetitive visual inspection of the fuel pump filter cover helicoil inserts and bolts for damage per SB72-126.; Terminating Action must be done at next engine or fule pump shop visit whichever occur first but not

This Ad is found terminated by installing a post SB 73-A129 MFP PN: 708600-5 SN:11251.Ref. UAL AD Compliance Records

73-A129 5, 5A, 5B, 5C WHICH COULD RESULT IN AN ENGINE FIRE AND DAAGE TO THE AIRPLANE

visit whichever occur first but not later than 5 yrs from the EOD of this AD by incorporating a D-bolt filter cover attachment per SB73-A129 or SB 73-125. (EOD: 2 Oct 2000)

on 17 Dec 2008.

19 2001-04-06 SB 72-854 R2 4-Apr-01CFM56 -3, 3B,

3CTO PREVENT FAN DISK FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINES FAILURE AND DAMAGE TO THE AIRPLANE.

T 21-Oct-97

Perform one time fan disk dovetail wear measurement per SB72-854R2. If required, perform a local ultrasonic inspection. (EOD: 4 April 2001). CAUTION: After the effective date of this AD, the following lubricants are no longer approved for use on the CFM56-3 series engine : Sandstrom 27A, ZIP D5460, Surf-Kote A1625, Tiolube 70, and Tiolube 75/75.

This AD is found incorporated previously by installing a post SB 72-854. Ref. UAL AD Compliance Records on 17 Dec 2008.

20 2001-11-05 SB 72-A0965 11-Jun-01CFM56 -2, 2B,3, 5B, 5C & 7B TO PREVENT NO.4 BEARING FAILURES, WHICH

COULD CAUSE AN ENGINE FAILUER. N/A

Remove the suspected no.4 bearing PN: 305-355-717-0 that has SN listed in Table 1 of this AD not later than 1 Jul 2001. CAUTION: After thte effective date of this AD , do not installany engine that has a No.4 bearing with serial number listed in the Table 1 of this Ad.

N/A No.4 Bearing PN installed.Ref. UAL AD Compliance Records on 17 Dec 2008.

Page 9: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

AS TO DATE : January 31, 2013ENGINE MODEL : CFM56-3C-1 TOTAL ENGINE TIME : 60137.57SERIAL NUMBER : 722283 TOTAL ENGINE CYCLES : 39308

SB REFERENCE ISSUENUMBER EFFECT. DATE HOURS CYCLES

APPLICABILITY NEXT DUE REMAIN METHOD OF COMPLIANCESTATUS INTERVALLAST ACCOMPLISHED

AIRWORTHINESS DIRECTIVE COMPLIANCE STATUSENGINE

FAA AD NO.NO DESCRIPTION REMARKS

21 2002-13-03 ESM 72-21-03 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

FAN DISK (ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

FPI, Disk Bore and Dovetail Eddy Current Inspection (ECI). Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

Fan Disk SN: BC779802

22 2002-13-03 ESM 72-22-01 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

FAN SHAFT(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

Magnetic Particle Inspection (MPI). Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

Fan Shaft SN: DE172092

23 2002-13-03 ESM 72-52-02 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5 5B 5C 7B

HPT DISK(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN O

NEXT PIECE PART

FPI, Disk Bore and Dovetail Eddy Current Inspection (ECI). Perform inspection at each piece-part opportunity in accordance HPT Disk SN: GWN0G150 5, 5B, 5C, 7B UNCONTAINED ENGINE FAILURE AND DAMAGE TO

THE AIRPLANE. OPPORTUN

ITY

part opportunity in accordance with the Inspection/Check section instruction.

24 2002-13-03 ESM 72-52-03 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPT FRONT ROTATING AIRSEAL(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

FPI, Seal Bore ECI and Bolt holes ECI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

Front Rotating Airseals SN: XAEJ5204

25 2002-13-03 ESM 72-31-04 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPC STAGE 1-2 SPOOL(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

R 20-Jan-08 7270 4587

NEXT PIECE PART

OPPORTUNITY

FPI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

HPC S 1-2 Spool SN: GWN09811 - CRACK FREE

26 2002-13-03 ESM 72-31-05 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPC STAGE 3 DISK(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

FPI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

HPC S 3 Disk SN: XAEH5648

27 2002-13-03 ESM 72-31-06 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPC STAGE 4-9 SPOOL(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

FPI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

HPC 4-9 Spool SN: GWN0GMF5

28 2002-13-03 ESM 72-31-07 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPC FRONT SHAFT(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

FPI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

HPC Front Shaft SN: GWN0FL01

29 2002-13-03 ESM 72-31-08 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

HPC REAR (CDP) AIRSEAL(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

FPI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

HPC RR seal SN: GFF5E4NJ

Page 10: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

AS TO DATE : January 31, 2013ENGINE MODEL : CFM56-3C-1 TOTAL ENGINE TIME : 60137.57SERIAL NUMBER : 722283 TOTAL ENGINE CYCLES : 39308

SB REFERENCE ISSUENUMBER EFFECT. DATE HOURS CYCLES

APPLICABILITY NEXT DUE REMAIN METHOD OF COMPLIANCESTATUS INTERVALLAST ACCOMPLISHED

AIRWORTHINESS DIRECTIVE COMPLIANCE STATUSENGINE

FAA AD NO.NO DESCRIPTION REMARKS

30 2002-13-03 ESM 72-54-03 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

LPT STAGE 1 DISK(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

FPI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

LPT S 1 Disk SN: DA353224

31 2002-13-03 ESM 72-54-03 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

LPT STAGE 2 DISK(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

FPI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

LPT S 2 Disk SN: BB370972

32 2002-13-03 ESM 72-54-03 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

LPT STAGE 3 DISK(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

FPI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

LPT S 3 Disk SN: BB345214

CFM56 -2 2A LPT STAGE 4 DISK(ALL PART NUMBER) . TO PREVENT NEXT FPI. Perform inspection at each

33 2002-13-03 ESM 72-54-03 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

OPIECE PART

OPPORTUNITY

piece-part opportunity in accordance with the Inspection/Check section instruction.

LPT S 4 Disk SN: BA467746

34 2002-13-03 ESM 72-54-05 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

LPT ROTOR SUPPORT(ALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

FPI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

LPT Rotor Support SN: DA352797

35 2002-13-03 ESM 72-55-01 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

LPT SHAFTALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

FPI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

LPT Shaft SN: LA075390

36 2002-13-03 ESM 72-55-02 1-Aug-02

CFM56 -2, 2A,2B, 3, 3B, 3C,5, 5B, 5C, 7B

LPT STUB SHAFTALL PART NUMBER) . TO PREVENT CRITICAL LIFE-LIMITED PARTS ROTATING ENGINE PART FAILURE, WHICH COULD RESULT IN AN UNCONTAINED ENGINE FAILURE AND DAMAGE TO THE AIRPLANE.

O

NEXT PIECE PART

OPPORTUNITY

FPI. Perform inspection at each piece-part opportunity in accordance with the Inspection/Check section instruction.

LPT Stub Shaft SN: BB387366

37 2004-10-13

73-A12973-087

73-0120 R5 24-Jun-04

CFM56 -2-C, -3Series & -5

Series.

TO PREVENT MAIN FUEL PUMP BEARING FAILURES RESULTING IN FUEL NOZZLE CLOGGING, LOW PRESSURE TURBINE (LPT) CASE BURN-THROUGH, AND DAMAGE TO THE AIRPLANE.

T 5-Aug-05

Remove the affected MFP for incorporating of SB73-120R5 at next engine shop visit, or main fule pump repair shop, whichever is earlier but not later than 1 Jan 2007.

Found Incorporated Previously. Perform accordance with SB 73-0120.Ref. UAL AD Compliance Records on 17 Dec 2008.

38 2006-26-01 73-141 1-Mar-07

CFM56 -2-C, -3Series, -5Series, -7B

Series.

TO PREVENT THE LOSS OF ENGINE THRUST THAT COULD RESULT IN LOSS OF CONTROL DURING TAKEOFF OR LANDING BY REPLACING THE DEFECTIVE/AFFECTED FUEL FILTER ELEMENTS

T 27-Apr-07

Remove the affected fuel filter, Western Filters PN: WF337881 or WF337017 and PTI Technologies PN: 7595983-101 or 7588133 and replace with filter that has PN not listed in this AD, but not later than 03 Jan 2007.

Found Incorporated Previously.Ref. UAL AD Compliance Records on 17 Dec 2008.

Page 11: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the
Page 12: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 14 of 55

Accessory Component List

ESN : 722283 TSN : 58410:95 CSN : 37957

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

1 N1 SPEED SENSOR

PN CFMI: 320-094-001-0

PN CFMI: 320-094-001-0

Original

320-094-001-0 / IPC 72-00-00-01,070 SN: 13057 SN: 13057

2 ALTERNATOR STATOR

PN CFMI: 74M802P03

PN CFMI: 74M802P03

Original

9974M82P03 / IPC 71-11-20-01,010A SN: GJAG5514 SN: GJAG5514

3 ALTERNATOR ROTOR

PN CFMI:

PRESENT

PN CFMI:

Original

9974M83P01 / IPC 72-00-00-15,620 SN: SN:

4 OIL TANK ASSY

PN CFMI: 335-261-203-0

PN CFMI: 335-261-203-0

Original

(335-261-203-0) IPC 72-23-00-09,200 SN: 2143 SN: 2143

5 INDICATOR CAP ASSY

PN CFMI: 335-260-905-0

PN CFMI: 335-260-905-0

Original

(335-260-905-0) / IPC 79-11-10-01,350 SN: 2205 SN: 2205

Page 13: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 15 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

6 LUBRICATION UNIT

PN CFMI:

PRESENT

PN CFMI:

Original

(335-261-00) / IPC 72-00-00-22,800 SN: SN:

7 OIL SCAVENGE FILTER

PN CFMI:

PRESENT

PN CFMI:

Original

(335-260-70) / IPC 72-00-00-22,851 SN: SN:

8 CHIP DETECTOR ( PLUG ASSY )

PN CFMI:

PRESENT

PN CFMI:

Original

(335-296-301-0) / IPC 79-21-10-01,120 SN: SN:

9 FUEL NOZZLE (X20)

PN CFMI:

PRESENT

PN CFMI:

Original

(9321M92G__) / IPC 73-11-40-01A,10 SN: SN:

10 VSV (LEFT)

PN CFMI: 1521M72P01

PN CFMI: 1521M72P01

Original

(1457M11P01) / IPC 72-00-02-15A,092 SN: APMBT083 SN: APMBT083

11 VSV (RIGHT)

PN CFMI: 1521M72P01

PN CFMI: 1521M72P01

Original

(1457M11P01) / IPC 72-00-02-20A,092 SN: APMBT203 SN: APMBT203

12 VSV FEEDBACK CABLE

PN CFMI: 9339M12P03

PN CFMI: 9339M12P03

Original

(9339M12P04) / IPC 72-00-00-06,730 SN: CCIAN955 SN: CCIAN955

Page 14: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 16 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

13 FUEL PUMP

PN CFMI: 301-779-005-0

PN CFMI: 301-779-005-0

Original

(301-779-005-0) / IPC 72-00-00-15,556 SN: 17869 SN: 17869

14 OIL/ FUEL HEAT EXCHANGER

PN CFMI: 301-776-401-0

PN CFMI: 301-776-401-0

Original

(301-776-403-0) / IPC 72-00-00-22,851 SN: 11687 SN: 11687

15 SERVO FUEL HEATER

PN CFMI: 301-776-501-0

PN CFMI: 301-776-501-0

Original

(301-776-501-0) / 72-00-00-22,710 SN: FHS11628 SN: FHS11628

16 MASTER BALLSCREW ACTUATOR

PN CFMI:

PRESENT

PN CFMI:

Original

(301-797-501-0) / IPC 72-23-00-23,696 SN: SN:

17 FLEXIBLE MAIN SHAFT

PN CFMI:

PRESENT

PN CFMI:

Original

(301-772-101-0) / IPC 72-23-00-23,610 SN: SN:

18 BLEED STOP MECHANISM

PN CFMI:

PRESENT

PN CFMI:

Original

(301-772-60__) / IPC 72-23-00-23,704 SN: SN:

19 HYDRAULIC GEAR MOTOR

PN CFMI: 706400-4

PN CFMI: 706400-4

Original

(301-776-70__) / IPC 72-31-10-01,10 SN: 13913 SN: 13913

Page 15: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 17 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

20 VBV FEEDBACK CABLE

PN CFMI:

PRESENT

PN CFMI:

Original

(301-812-601-0) / IPC 72-00-00-06,440 SN: SN:

21 BALLSCREW ACTUATOR (X11)

PN CFMI:

PRESENT

PN CFMI:

Original

(301-792-30 __) / IPC 72-23-00-23 SN: SN:

22 FLEXIBLE SHAFT ASSY (X11)

PN CFMI:

PRESENT

PN CFMI:

Original

(301-774-201-0) / IPC 72-23-00-23,742 SN: SN:

23 EGT LEFT UPPER WIRING HARNESS

PN CFMI: 301-778-001-0

PN CFMI: 301-778-001-0

Original

( TC 174-00 ) / IPC 72-00-00-31A,020 SN: 4C231154 SN: 4C231154

24 EGT LEFT LOWER WIRING HARNESS

PN CFMI:

PRESENT

PN CFMI:

Original

( TC 174-00 ) / IPC 72-00-00-31A,021 SN: SN:

25 EGT LOWER (CONNECTOR) WIRING HARNESS

PN CFMI: 301-780-301-0

PN CFMI: 301-780-301-0

Original

( CA 152-00 ) / IPC 72-00-00-31A,130 SN: 11065 SN: 11065

26 EGT (UPPER) CONNECTOR) WIRING HARNESS

PN CFMI: 301-785-001-0

PN CFMI: 301-785-001-0

Original

( CA 150-00 ) / IPC 72-00-00-31A,510 SN: 10875 SN: 10875

Page 16: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 18 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

27 EGT RH WIRING HARNESS

PN CFMI: 301-785-101-0

PN CFMI: 301-785-101-0

Original

( TC 200-00 ) / IPC 72-00-00-31A,640 SN: 16921 SN: 16921

28 EGT FWD (CONNECTOR) WIRING HARNESS

PN CFMI: 301-784-201-0

PN CFMI: 301-784-201-0

Original

( CA 150-00 ) / IPC 72-00-00-31A,700 SN: 12099 SN: 12099

29 T12 TEMPERATURE SENSOR

PN CFMI: 301-771-601-0

PN CFMI: 301-771-601-0

Original

(301-771-601-0) / IPC 72-00-00-06,790 SN: 06686 SN: 06686

30 BLEED FLOW SENSOR ASSY( BIAS SENSOR)

PN CFMI:

PRESENT

PN CFMI:

Original

(7082M47G07) / IPC 75-00-00-31-10 SN: SN:

31 T2 SENSOR

PN CFMI: 9375M82P04

PN CFMI: 9375M82P04

Original

(9375M82P04) / IPC 73-21-25-01,10 SN: WYG-56643 SN: WYG-56643

32 CIT SENSOR

PN CFMI:

PRESENT

PN CFMI:

Original

(9334M96P02) / IPC 72-00-00-02,260 SN: SN:

33 BEARING VIBRATION SENSOR

PN CFMI:

PRESENT

PN CFMI:

Original

(301-776-90 __) / IPC 72-00-01-01,090 SN: SN:

Page 17: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 19 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

34 VIBRATION (TRF) SENSOR

PN CFMI:

PRESENT

PN CFMI:

Original

(301-779-303-0) / IPC 72-00-00-82,010 SN: SN:

35 IGNITION UNIT (LEFT) EXCITER (UP)

PN CFMI: 9238M66P08

PN CFMI: 9238M66P08

Original

(9238M66P07) IPC 72-00-00-04,580 SN: UNJI6045 SN: UNJI6045

36 IGNITION UNIT (RIGHT) EXCITER ( LOW )

PN CFMI: 9238M66P07

PN CFMI: 9238M66P07

Original

(9238M66P07) / IPC 72-00-00-04,730 SN: BND4607K SN: BND4607K

37 IGNITION LH LEAD ASSY

PN CFMI: CII53552-2

PN CFMI: CII53552-2

Original

(9339M26P14) / IPC 72-00-00-04,720 SN: 6023271 SN: 6023271

38 IGNITION RH LEAD ASSY

PN CFMI: CII55552-2

PN CFMI: CII55552-2

Original

(9339M26P13) / IPC 72-00-00-04,570 SN: 05020251 SN: 05020251

39 MAIN SPARK IGNITER (LEFT)

PN CFMI:

PN CFMI: CH31900-6

NEW

(1374M12P01) / IPC 72-00-00-04,801 SN: 01003652 SN: 01003652

40 MAIN SPARK IGNITER (RIGHT)

PN CFMI: CH31900-6

PN CFMI:

Original

(1374M12P01) / IPC 72-00-00-04,801 SN: 01003652 SN:

Page 18: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 20 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

41 ACCESSORY GEARBOX ASSY

PN CFMI: 335-300-108-0

PN CFMI: 335-300-108-0

Original

(335-300-110-0) / IPC 72-63-00 SN: 3107 SN: 3107

42 TRANSFER GEARBOX

PN CFMI: 335-300-611-0

PN CFMI: 335-300-611-0

Original

335-300-010-0) / IPC 72-62-00 SN: VB-3064 SN: VB-3064

43 TURBINE CLEARANCE VALVE (HPTCCV)

PN CFMI: NOT VISIBLE

PN CFMI: NOT VISIBLE

Original

7061M31G05) / IPC 72-00-02-35,010 SN: MR7525 SN: MR7525

44 HPTCC TIMER ASSY

PN CFMI: NOT VISIBLE

PN CFMI: NOT VISIBLE

Original

(7119M71G07) / IPC 72-00-00-86,10 SN: G087XXX SN: G087XXX

45 ELECTRO VALVE TCC TIMER

PN CFMI:

PRESENT

PN CFMI:

Original

(301-787-401-0) / IPC 72-00-00-84,901 SN: SN:

46 STARTING BLEED AIR VALVE

PN CFMI:

PRESENT

PN CFMI:

Original

(1527M90P01) / IPC 75-21-20-01,10 SN: SN:

47 POWER MANAGEMENT CONTROL

PN CFMI: 7147M10G03

PN CFMI: 7147M10G03

Original

7147M10G04) / IPC72-00-00-04,460 SN: ECDB5086 SN: ECDB5086

Page 19: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 21 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

48 WIRING CONTROL HARNESS

PN CFMI: 320-500-403-0

PN CFMI: 320-500-403-0

Original

(320-500-403-0) / IPC 72-00-00-04,230 SN: YN588057-2 SN: YN588057-2

49 ELECTRICAL ALTERNATOR LEAD ASSY

PN CFMI: 320-112-001-0

PN CFMI: 320-112-001-0

Original

(320-112-001-0) / IPC 72-00-00-04,320 SN: 12513 SN: 12513

50 MAIN ENGINE CONTROL

PN CFMI: 8063-214

PN CFMI: 8063-215

OVH

1459M27P05) / IPC72-00-00-15,530 SN: 11491372 SN: WYG43875

51 LEFT THRUST LINK FITTING

PN CFMI:

PRESENT

PN CFMI:

Original

310A1036- __) / PPBU 71-00-02-2-1,5 SN: SN:

52 LEFT FAN CASE SUPPORT ASSY( FWD MOUNT)

PN CFMI:

PRESENT

PN CFMI:

Original

(310A1020 __) / PPBU 71-00-02-2- SN: SN:

53 CONE BOLT LEFT

PN CFMI: 310A1041-5

PN CFMI: 310A1041-5

Original

(310A1041-5) / PPBU 71-00-02-2- SN: 7684 SN: 7684

54 RIGHT THRUST LINK FITTING

PN CFMI:

PRESENT

PN CFMI:

Original

(310A1036-__) / PPBU 71-00-02-2-2,5 SN: SN:

Page 20: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 22 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

55 RIGHT FAN CASE SUPPORT ASSY

PN CFMI:

PRESENT

PN CFMI:

Original

(310A1020- __) / PPBU 71-00-02-2-2,30 SN: SN:

56 CONE BOLT RIGHT

PN CFMI: 310A1041-5

PN CFMI: 310A1041-5

Original

(310A1041-5) / PPBU 71-00-02-2- SN: 5/28/1916 SN: 5/28/1916

57 THRUST LINK ASSY

PN CFMI: 310A1026-1

PN CFMI: 310A1026-1

Original

(310A1020- __) / PPBU 71-00-00-03,10 SN: 22418 SN: 22418

58 AFT MOUNT ASSY

PN CFMI: 310A103-2

PN CFMI: 310A103-2

Original

(310A1020-26) / PPBU 71-00-02-2-3,30 SN: 598 SN: 598

59 OUTER RING SEGMENT

PN CFMI:

PRESENT

PN CFMI:

Original

(333A1120-__) / IPC 78-30-00-51,370 SN: SN:

60 STRUT ASSY

PN CFMI:

PRESENT

PN CFMI:

Original

(333A1150-3 ) / IPC 78-30-00-51,205 SN: SN:

61 FAN AIR/ PRECOOLER CONTROL VALVE

PN CFMI: 10-62008

PN CFMI: 10-62008

Original

(10-62008-__) / PPBU 71-00-02-8-4,5 SN: 3039 SN: 3039

Page 21: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 23 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

62 INNER RING SEGMENT

PN CFMI:

PRESENT

PN CFMI:

Original

(333A1130-3) SN: SN:

63 DEFLECTOR ASSY

PN CFMI: 332A1988-39

PN CFMI: 332A1988-39

Original

(332A1908-58) SN: NOT VISIBLE SN: NOT VISIBLE

64 FUEL FLOW TRANSMITTER

PN CFMI: S347T001-6

PN CFMI: S347T001-6

Original

(S347T001-6) SN: 131389 SN: 131389

65 FUEL SUPPLY INLET LINE

PN CFMI: S332A004-2

PN CFMI: S332A004-2

Original

(S332A004-2) SN: NOT VISIBLE SN: NOT VISIBLE

66 FUEL FILTER DIFFERENTIAL PRESSURE SWITCH

PN CFMI:

PRESENT

PN CFMI:

Original

(S332T004-7) / PPBU 71-00-02-7-3,5 SN: SN:

68 BLEED AIR REGULATOR

PN CFMI:

MISSING

PN CFMI: 107492-3

OVH

(10-62008-__) / PPBU 71-00-02-8-1,5 SN: SN: 7055

69 HIGH STAGE REGULATOR

PN CFMI: 10-62008-39

PN CFMI: 10-62008-39

Original

(10-62008-__) / PPBU 71-00-02-8-1,310 SN: 7709 SN: 7709

Page 22: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 24 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

70 PRSOV

PN CFMI: 10-62008-30

PN CFMI: 10-62008-30

Original

(10-62008-30) / PPBU 71-00-02-8-5,5 SN: 1394 SN: 1394

71 DUCT ASSY

PN CFMI: S32A003-5

PN CFMI: S32A003-5

Original

(332A1327-__) SN: NOT VISIBLE SN: NOT VISIBLE

72 DUCT ASSY, UPPER 5TH STAGE

PN CFMI:

PRESENT

PN CFMI:

Original

(332A1320-1) SN: SN:

73 5th STAGE BLEED CHECK VALVE

PN CFMI: 3202222-1

PN CFMI: 3202222-1

Original

(10-62008-1) PPBU 71-00-02-8-2,65 SN: 4068 SN: 4068

74 LOWER 5TH STAGE BLEED DUCT SEGMENT

PN CFMI: S332A003-15

PN CFMI: S332A003-15

Original

(332A1304-24) SN: 239 SN: 239

75 LEFT 9TH STAGE BLEED DUCT SEGMENT

PN CFMI: 332A1305-9

PN CFMI: 332A1305-9

Original

(332A1305-9) SN: NOT VISIBLE SN: NOT VISIBLE

76 9TH STAGE BLEED DUCT SEGMENT

PN CFMI: 332A003-4

PN CFMI: 332A003-4

Original

(332A1330-1) SN: 48549 SN: 48549

Page 23: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 25 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

77 HIGH STAGE/ HIGH PRESSURE SHUTOFF VALVE

PN CFMI: 10-62008-32

PN CFMI: 10-62008-32

Original

(10-62008-__) / PPBU 71-00-02-8-3,175 SN: 7267 SN: 7267

78 RIGHT 9TH STAGE BLEED DUCT

PN CFMI: 332AXXX

PN CFMI: 332AXXX

Original

(332A1311-30) SN: NOT VISIBLE SN: NOT VISIBLE

79 OIL PRESSURE TRANSMITTER

PN CFMI: 418-20049

PN CFMI: 418-20049

Original

(418-20044) SN: 3302644 SN: 3302644

80 LOW OIL PRESSURE WARNING SWITCH

PN CFMI: 21SN04-211A

PN CFMI: 21SN04-211A

Original

(10-3269-12) / IPC 79-30-00-76-195 SN: U212B SN: U212B

81 OIL FILTER DIFFERENT PRESSURE SWITCH

PN CFMI:

PRESENT

PN CFMI:

Original

(10-3269-13) / IPC 79-30-00-76-460 SN: SN:

82 OIL TEMPERATURE TRANSMITTER

PN CFMI:

PRESENT

PN CFMI:

Original

(1122514 / PPBU 71-00-02-9-3,125 SN: SN:

83 OIL QUANTITY TRANSMITTER

PN CFMI: 10-60722-11

PN CFMI: 10-60722-11

Original

(10-60722-11) / PPBU 71-00-02-8-1,310 SN: 2343 SN: 2343

Page 24: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 26 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

84

(341A1010-__) SN: SN:

85 SKIRT FAIRING

PN CFMI:

PRESENT

PN CFMI:

Original

(314A1502-42) SN: SN:

86 PRIMARY EXHAUST SLEEVE

PN CFMI:

PRESENT

PN CFMI:

Original

(314A1502-__) / PPBU 71-00-02-11-1,45 SN: SN:

87 EXHAUST PLUG

PN CFMI:

PRESENT

PN CFMI:

Original

(3141501-__) / PPBU 71-00-02-11-1,25 SN: SN:

88 AC GENERATOR

PN CFMI:

MISSING

PN CFMI: 976J498-1

OVH

(10-61224-12) SN: SN: YC7582M

89 CONSTANT SPEED DRIVE

PN CFMI:

MISSING

PN CFMI: 735511A

OVH

(10-61066-11) / PPBU 71-00-02-12-1,45 SN: SN: B0655

90 QAD KIT

PN CFMI:

MISSING

PN CFMI: 10-60295-15

OVH

(10-60295-15) SN: SN: BTV3976

Page 25: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 27 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

91 CSD OIL COOLER

PN CFMI:

PRESENT

PN CFMI:

Original

(10-61233-11) / PPBU 71-00-02-12-3,5 SN: SN:

92 CSD COOLING OIL TEMPERATURE SWITCH

PN CFMI:

PRESENT

PN CFMI:

Original

(332A1207-1) / PPBU 71-00-02-12-4,75 SN: SN:

93 CSD COOLING OIL FILTER

PN CFMI:

PRESENT

PN CFMI:

Original

(7581418) SN: SN:

94 DUCT SEGMENT

PN CFMI:

PRESENT

PN CFMI:

Original

(332A1200-3) SN: SN:

95 ADAPTER

PN CFMI:

PRESENT

PN CFMI:

Original

(332A1025-2) SN: SN:

96 DUCT SEGMENT GENERATOR

PN CFMI:

PRESENT

PN CFMI:

Original

(332A1200-__) SN: SN:

97 DUCT COUPLER

PN CFMI:

PRESENT

PN CFMI:

Original

(BACD40D8-12-30) SN: SN:

Page 26: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 28 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

98 DUCT COUPLER

PN CFMI:

PRESENT

PN CFMI:

Original

(BACD40D10-12-30) SN: SN:

99 TERMINAL BOARD

PN CFMI:

PRESENT

PN CFMI:

Original

(332A1023-47) SN: SN:

100 CURRENT TRANSFORMER

PN CFMI: 10-61224-5

PN CFMI: 10-61224-5

Original

(10-61224-5) SN: RJ7769 SN: RJ7769

101 DUCT ASSY

PN CFMI: S332A003-4

PN CFMI: S332A003-4

Original

(332A1301-1) SN: NSN SN: NSN

102 START VALVE

PN CFMI: 3289XXX

PN CFMI: 3289XXX

Original

(S332A002-__) / IPC 72-00-02-35,620 SN: 2103 SN: 2103

103 STARTER

PN CFMI:

MISSING

PN CFMI: 3505716-6

OVH

(S332A001-__) SN: SN: 535C

104 STARTER ADAPTER

PN CFMI:

PRESENT

PN CFMI:

Original

(S332A001-2) SN: SN:

Page 27: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 29 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

105 HYDRAULIC PUMP

PN CFMI: 10-61794-2

PN CFMI: 10-61794-2

Original

(10-61794-1) / PPBU 71-00-02-13-2,315 SN: MX4383XX SN: MX4383XX

106 ADAPTER PLATE

PN CFMI:

PRESENT

PN CFMI:

Original

(387999) SN: SN:

107 HYDRAULIC SUPPLY HOSE

PN CFMI: S332A005-15

PN CFMI: S332A005-15

Original

(S332A005-15) SN: 1189 SN: 1189

108 HYDRAULIC PRESSURE HOSE

PN CFMI: S332A00-5

PN CFMI: S332A00-5

Original

(S332A005-12) SN: 0712 SN: 0712

109 HYDRAULIC CASE DRAIN HOSE

PN CFMI: S332A005-17

PN CFMI: S332A005-17

Original

(S332A005-17) SN: 1014 SN: 1014

110 DUCT INSULATION

PN CFMI: S332A104-10

PN CFMI: S332A104-10

Original

(S332A104-__) SN: M424330-001 SN: M424330-001

111 TAI VALVE ASSY

PN CFMI:

MISSING

PN CFMI: 79318-321209-3

OVH

(S332A101-__) / PPBU 71-00-02-15-1,55 SN: SN: 39982-37

Page 28: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 30 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

112 TAI PRESSURE SWITCH

PN CFMI: NOT VISIBLE

PN CFMI: NOT VISIBLE

Original

(21SN41-52) / PPBU 71-00-02-15-1,125 SN: K343 SN: K343

113 DUCT INSULATION

PN CFMI:

MISSING

PN CFMI:

A/C SIDE

(S332A104-9) SN: SN:

114 TEMPERATURE SWITCH

PN CFMI:

MISSING

PN CFMI:

A/C SIDE

(17343-116-825R) SN: SN:

115 FIRE DETECTOR - REAR

PN CFMI: S332T101-3

PN CFMI: S332T101-3

Original

(S332T101-3) / PPBU 71-00-02-16-1,15 SN: 0030 SN: 0030

116 FIRE DETECTOR - LOWER

PN CFMI:

PRESENT

PN CFMI:

Original

(S332T101-1) / PPBU 71-00-02-16-1,10 SN: SN:

117 FIRE DETECTOR - UPPER

PN CFMI: S332T101-2

PN CFMI: S332T101-2

Original

(S332T101-2) SN: 3305 SN: 3305

118 W 1502 WIRE BUNDLE ASSY

PN CFMI:

PRESENT

PN CFMI:

Original

(61-31502) SN: SN:

Page 29: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 31 of 55

IN OUT

NO DESCRIPTION (TYPICAL PN) CHECK LISTING INCOMING REMARK CHECK LISTING OUT

GOING REMARK

119 W 1504 WIRE BUNDLE ASSY

PN CFMI:

PRESENT

PN CFMI:

Original

(61-31504) SN: SN:

120 W 1506 WIRE BUNDLE ASSY

PN CFMI:

PRESENT

PN CFMI:

Original

(61-31506) SN: SN:

121 W 0200 WIRE BUNDLE ASSY

PN CFMI:

PRESENT

PN CFMI:

Original

(61-30200) / PPBU 71-00-02-18-2,45 SN: SN:

122 W 1508 WIRE BUNDLE ASSY

PN CFMI:

PRESENT

PN CFMI:

Original

(61-31508) / PPBU 71-00-02-18-5,5 SN: SN:

Page 30: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 55 of 55

Page 31: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the
Page 32: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the
Page 33: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 050112-050912_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 05/10/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 05/10/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112 * . G . F X 2 . -999.99 105 50 0 050112 * . G . F X 2 . -999.99 100 48 1 050112 * . G . F X 2 . -999.99 105 50 0 050212 * . G . F X 2 . -999.99 110 47 1 050212 * . G . F X 2 . -999.99 100 48 1 050212 * . G . F X 2 . -999.99 110 50 2 050212 * . G . F X 2 . -999.99 99 48 0 050312 * . G . F X 2 . -999.99 130 50 0 050312 * . G . F X 2 . -999.99 140 50 0 050312 * . G . F X 2 . -999.99 110 50 2 050312 * . G F . X 2 . -999.99 100 48 2 050312 * . G F . X 2 . -999.99 110 50 0 050312 * . G F . X 2 . -999.99 110 48 0 050312 * . G F . X 2 . -999.99 105 50 1 050312 * . G F . X 2 . -999.99 0 0 0 050412 * . G F . X 2 . -999.99 120 50 2 050412 * . G F . X 2 . -999.99 105 51 0 050412 * . G F . X 2. -999.99 105 50 1 050412 * . G F . X 2. -999.99 105 49 0 050412 * . G F . X 2 . -999.99 105 50 1 050512 * . G F . X 2 . -999.99 110 50 1 050512 * . G F . X 2 . -999.99 110 47 1 050512 * . G F . X 2 . -999.99 100 48 1 050512 * . G F X 2 . -999.99 95 48 1 050512 * . G F X 2 . -999.99 95 48 1 050612 * . G .F X 2 . -999.99 48 48 1 050612 * . G . F X 2 . -999.99 103 46 1 050612 * . G . F X 2 . -999.99 102 48 1 050812 * . G . F X 2 . -999.99 100 47 0 050812 * . G . F X 2 . -999.99 110 47 0 050812 * . G . F X 2 . -999.99 105 48 1 050812 * . G . F X 2 . -999.99 110 48 0 050812 * . G . F X 2 . -999.99 110 48 0 050812 * . G . F X 2 . -999.99 110 45 0 050912 * . G . F X 2 . -999.99 99 48 0 050912 * . G . F X 2 . -999.99 100 48 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 050612 * .G . F 2X . -999.99 1 050612 * . G . F X 2 . -999.99 1 050812 * X X X X -999.99 0 050812 * X X X X -999.99 0 050812 * G . F X2 . -999.99 1 050812 * . G . F X 2 . -999.99 0 050812 * . G . F X 2 . -999.99 0 050812 * G . F * . -999.99 0 050912 * X X X X -999.99 0 050912 * X X X X -999.99 0

Page 1

Page 34: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 051012-051912_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 05/21/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 05/21/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 051012 * . G . F X 2 . -999.99 102 50 2 051012 * . G . F X 2 . -999.99 110 48 1 051012 * . G . F X 2 . -999.99 110 48 1 051012 * . G . F X 2 . -999.99 100 50 1 051112 * . G . F X 2 . -999.99 110 44 1 051112 * . G . F X 2 . -999.99 105 48 1 051112 * . G . F X 2 . -999.99 105 48 0 051112 * . G . F X 2 . -999.99 105 50 1 051212 * . G . F X 2 . -999.99 100 48 1 051212 * . G . F X 2 . -999.99 120 48 1 051212 * . G . F X 2 . -999.99 120 48 0 051212 * . G . F X 2 . -999.99 100 48 1 051212 * . G . F X 2 . -999.99 105 48 1 051312 * . G . F X 2 . -999.99 110 48 1 051312 * . G . F X 2 . -999.99 100 48 1 051312 * . G . F X 2 . -999.99 110 47 0 051312 * . G . F X 2 . -999.99 110 48 0 051312 * . G . F X 2 . -999.99 110 50 2 051412 * . G . F X 2 . -999.99 110 50 1 051412 * . G . F X 2 . -999.99 110 48 0 051412 * . G . F X 2 . -999.99 110 48 0 051412 * . G . F X 2 . -999.99 100 50 0 051512 * . G . F X 2 . -999.99 110 48 0 051512 * . G . F X 2 . -999.99 100 48 1 051512 * . G . F X 2 . -999.99 105 48 0 051612 * . G . F X 2 . -999.99 110 45 0 051612 * . G . F X 2 . -999.99 110 50 0 051712 * . G . F X 2 . -999.99 105 48 1 051712 * . G . F X 2 . -999.99 101 48 1 051812 * . G . F X 2 . -999.99 120 49 2 051812 * . G . F X 2 . -999.99 95 49 1 051812 * . G . F X 2 . -999.99 110 50 1 051912 * . G . F X 2 . -999.99 105 48 1 051912 * . G . F X 2 . -999.99 105 46 1 051912 * . G . F X 2 . -999.99 120 50 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 051612 * -G . . F X 2 . -999.99 0 051612 * . -F G . X . 2 -999.99 0 051712 * . G . F 2 X . -999.99 1 051712 * . G . F X 2 . -999.99 1 051812 * . G F . X 2 . -999.99 2 051812 * . G F . X 2 . -999.99 1 051812 * . G F . X 2. -999.99 1 051912 * . G . F 2 X . -999.99 1 051912 * . G . F X 2 . -999.99 1 051912 * . G F . X 2 . -999.99 0

Page 1

Page 35: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 052012-053012_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 05/31/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 05/31/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) -20..-10....0...EGT..20...30...40 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 052012 * . G . F X 2 . -999.99 105 50 1 052112 * . G . F X 2 . -999.99 110 48 0 052112 * . G . F X 2 . -999.99 120 48 0 052112 * . G . F X 2 . -999.99 120 48 0 052112 * . G . F X 2 . -999.99 102 46 0 052212 * . G . F X 2 . -999.99 100 48 1 052212 * . G . F X 2 . -999.99 100 48 1 052312 * . G . F X 2 . -999.99 105 48 1 052312 * . G . F X 2 . -999.99 100 48 1 052312 * . G . F X 2 . -999.99 100 47 1 052312 * . G . F X 2 . -999.99 99 48 1 052312 * . G . F X 2 . -999.99 105 48 0 052312 * . G . F X 2 . -999.99 105 48 0 052412 * . G . F X 2 . -999.99 100 42 0 052412 * . G . F X 2 . -999.99 100 48 0 052412 * . G . F X 2 . -999.99 120 48 0 052512 * . G . F X 2 . -999.99 110 48 0 052512 * . G . F X 2 . -999.99 110 50 0 052512 * . G . F X 2 . -999.99 100 46 0 052612 * . G . F X 2 . -999.99 105 48 0 052612 * . G . F X 2 . -999.99 105 50 1 052612 * . G . F X 2 . -999.99 120 50 1 052612 * . G . F X 2 . -999.99 110 50 1 052712 * . G . F X 2 . -999.99 105 48 1 052712 * . G . F X 2 . -999.99 105 48 0 052712 * . G . F X 2 . -999.99 0 0 0 052712 * . G . F X 2 . -999.99 105 48 0 052812 * . G . F X 2 . -999.99 110 48 0 052812 * . G . F X 2 . -999.99 110 48 0 052812 * . G . F X 2 . -999.99 105 48 0 052912 * . G . F X 2 . -999.99 100 49 0 052912 * . G . F X 2 . -999.99 100 50 2 052912 * . G . F X 2 . -999.99 120 50 2 053012 * . G . F X 2 . -999.99 105 50 0 053012 * . G . F X 2 . -999.99 110 45 0 RAW DATA -20..-10....0...EGT..20...30...40 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 052712 * X X X X -999.99 0 052712 * . G . F X 2 . -999.99 0 052812 * . G . F X 2 . -999.99 0 052812 * . G . F X 2 . -999.99 0 052812 * . G .F X 2 . -999.99 0 052912 * . G . F X 2 . -999.99 0 052912 * . F G . X . 2 -999.99 2 052912 * . F G . X . 2 -999.99 2 053012 * . G . F X 2 . -999.99 0 053012 * . G . F X 2 . -999.99 0

Page 1

Page 36: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 053112-060512_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 06/07/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 06/07/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) -20..-10....0...EGT..20...30...40 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 053112 * . G . F X 2 . -999.99 110 46 0 053112 * . G . F X 2 . -999.99 120 50 0 053112 * . G . F X 2 . -999.99 120 50 0 053112 * . G . F X 2 . -999.99 110 46 0 060112 * . G . F X 2 . -999.99 105 48 0 060112 * . G . F X 2 . -999.99 110 48 0 060112 * . G . F X 2 . -999.99 110 48 0 060112 * . G . F X 2 . -999.99 100 48 0 060112 * . G . F X 2 . -999.99 105 48 0 060212 * . G . F X 2 . -999.99 105 47 1 060212 * . G . F X 2 . -999.99 105 48 1 060212 * . G . F X 2 . -999.99 105 48 0 060212 * . G . F X 2 . -999.99 100 48 0 060212 * . G . F X 2 . -999.99 100 50 1 060212 * . G . F X 2 . -999.99 100 50 1 060212 * . G . F X 2 . -999.99 100 48 0 060312 * . G . F X 2 . -999.99 100 48 0 060312 * . G . F X 2 . -999.99 110 48 1 060312 * . G . F X 2 . -999.99 105 46 1 060312 * . G . F X 2 . -999.99 105 46 0 060312 * . G . F X 2 . -999.99 110 48 0 060312 * . G . F X 2 . -999.99 110 48 0 060312 * . G . F X 2 . -999.99 100 43 1 060412 * . G . F X 2 . -999.99 105 43 1 060412 * . G . F X 2 . -999.99 110 48 0 060412 * . G . F X 2 . -999.99 104 48 0 060412 * . G . F X 2 . -999.99 102 48 0 060412 * . G . F X 2 . -999.99 106 47 0 060412 * . G . F X 2 . -999.99 105 47 1 060412 * . G . F X 2 . -999.99 100 48 0 060512 * . G . F X 2 . -999.99 110 48 0 060512 * . G . F X 2 . -999.99 100 48 0 060512 * . G . F X 2 . -999.99 110 48 0 060512 * . G . F X 2 . -999.99 100 48 0 060512 * . G . F X 2 . -999.99 110 47 0 RAW DATA -20..-10....0...EGT..20...30...40 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -4...-2....0...F/F...4....6....8 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 060412 * . G . F X 2 . -999.99 0 060412 * . G F. X 2 . -999.99 0 060412 * .G . F X 2 . -999.99 0 060412 * . G . F X 2 . -999.99 1 060412 * X X X X -999.99 0 060512 * . G . F X2 . -999.99 0 060512 * . G .F X 2 . -999.99 0 060512 * . G . F X 2 . -999.99 0 060512 * . G . F X 2 . -999.99 0 060512 * . G . F * . -999.99 0

Page 1

Page 37: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 060612-061212_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 06/13/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 06/13/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) -20..-10....0...EGT..20...30...40 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 060112C * . G . F X 2 . -999.99 -5 -5 0 060612 * . G . F X 2 . -999.99 100 48 0 060612 * . G . F X 2 . -999.99 105 48 1 060712 * . G . F X 2 . -999.99 105 48 1 060712 * . G . F X 2 . -999.99 105 48 0 060712 * . G . F X 2 . -999.99 105 45 0 060812 * . G . F X 2 . -999.99 120 47 0 060812 * . G . F X 2 . -999.99 110 50 2 060812 * . G . F X 2 . -999.99 110 50 1 060812 * . G . F X 2 . -999.99 100 45 0 060812 * . G . F X 2 . -999.99 105 46 1 060812 * . G . F X 2 . -999.99 105 48 1 060812 * . G . F X 2 . -999.99 100 0 2 060912 * . G . F X 2 . -999.99 120 48 0 060912 * . G . F X 2 . -999.99 102 46 0 060912 * . G . F X 2 . -999.99 120 48 0 060912 * . G . F X 2 . -999.99 110 49 0 060912 * . G . F X 2 . -999.99 110 48 1 060912 * . G . F X 2 . -999.99 99 48 0 061012 * . G . F X 2 . -999.99 110 48 1 061012 * . G . F X 2 . -999.99 102 49 0 061012 * . G . F X 2 . -999.99 0 0 0 061012 * . G . F X 2 . -999.99 100 48 0 061012 * . G . F X 2 . -999.99 99 48 1 061012 * . G . F X 2 . -999.99 100 48 0 061112 * . G . F X 2 . -999.99 110 48 0 061112 * . G . F X 2 . -999.99 102 46 1 061112 * . G . F X 2 . -999.99 105 50 2 061112 * . G . F X 2 . -999.99 105 50 1 061112 * . G . F X 2 . -999.99 103 45 0 061112 * . G . F X 2 . -999.99 102 45 0 061212 * . G . F X 2 . -999.99 110 46 0 061212 * . G . F X 2 . -999.99 105 50 0 061212 * . G -F . X 2 . -999.99 102 48 0 061212 * . G -F . X 2 . -999.99 120 48 0 RAW DATA -20..-10....0...EGT..20...30...40 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 061112 * .G . F X 2 . -999.99 0 061112 * G . F 2X . -999.99 1 061112 * . G F . X 2 . -999.99 2 061112 * . G F . X 2 . -999.99 1 061112 * . G F. X 2 . -999.99 0 061112 * . G . F X2 . -999.99 0 061212 * . G . F X 2 . -999.99 0 061212 * . +* . X .2 -999.99 0 061212 * . G -F . X 2 . -999.99 0 061212 * . G . F X 2 . -999.99 0

Page 1

Page 38: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 061312-061912_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 06/28/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 06/28/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 060112C * . G . F X 2 . -999.99 -5 -5 0 061312 * . G F . X 2 . -999.99 105 46 2 061312 * . G F . X 2 . -999.99 102 44 2 061312 * . G F . X 2 . -999.99 120 49 1 061312 * . G F . X 2 . -999.99 102 49 1 061312 * . G F . X 2 . -999.99 105 48 1 061312 * . G F . X 2 . -999.99 110 48 1 061412 * . G F . X 2 . -999.99 105 45 1 061412 * . G F . X 2 . -999.99 102 45 1 061412 * . G F . X 2 . -999.99 102 45 1 061512 * . G F . X 2 . -999.99 100 48 1 061512 * . G F . X 2 . -999.99 110 50 0 061512 * . G F . X 2 . -999.99 100 48 1 061512 * . G F . X 2 . -999.99 110 48 1 061512 * . G F . X 2 . -999.99 110 48 1 061512 * . G F . X 2 . -999.99 105 50 0 061512 * . G F . X 2 . -999.99 110 48 1 061512 * . G F . X 2 . -999.99 105 45 0 061612 * . G F . X 2 . -999.99 100 46 0 061612 * . G F . X 2 . -999.99 110 48 0 061612 * . G F . X 2 . -999.99 100 48 1 061612 * . G F . X 2 . -999.99 100 51 1 061712 * . G F . X 2 . -999.99 90 47 0 061712 * . G F . X 2 . -999.99 110 40 1 061712 * . G F . X 2 . -999.99 115 48 0 061812 * . G F . X 2 . -999.99 110 48 0 061812 * . G F . X 2 . -999.99 110 49 0 061812 * . G F . X 2 . -999.99 105 50 0 061812 * . G F . X 2 . -999.99 105 50 0 061912 * . G F . X 2 . -999.99 110 48 0 061912 * . G F . X 2 . -999.99 110 49 0 061912 * . G F . X 2 . -999.99 110 50 0 061912 * . G F . X 2 . -999.99 110 48 0 061912 * . G F . X 2 . -999.99 110 48 0 061912 * . G F . X 2 . -999.99 110 50 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 061812 * . G .F X 2 . -999.99 0 061812 * . G F X 2 . -999.99 0 061812 * . G . F X 2 . -999.99 0 061812 * . G F . X 2 . -999.99 0 061912 * . G F . X 2 . -999.99 0 061912 * . G F . X 2 . -999.99 0 061912 * . G F. X 2 . -999.99 0 061912 * . G F . X 2 . -999.99 0 061912 * . G F . X 2 . -999.99 0 061912 * . G F . X . 2 -999.99 0

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Page 39: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 062012-062612_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 07/05/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 07/05/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 060112C * . G . F X 2 . -999.99 -5 -5 0 062012 * . G F . X 2 . -999.99 105 50 0 062012 * . G F . X 2 . -999.99 110 50 0 062012 * . G F . X 2 . -999.99 110 47 0 062012 * . G F . X 2 . -999.99 110 50 0 062012 * . G . F X 2 . -999.99 110 50 1 062012 * . G . F X 2 . -999.99 120 50 0 062012 * . G . F X 2 . -999.99 110 50 0 062012 * . G . F X 2 . -999.99 110 48 0 062112 * . G . F X 2 . -999.99 110 48 0 062112 * . G . F X 2 . -999.99 119 48 0 062112 * . G .F X 2 . -999.99 105 50 0 062212 * . G .F X 2 . -999.99 110 48 0 062312 * . G .F X 2 . -999.99 110 50 0 062312 * . G F X 2 . -999.99 105 50 0 062312 * . G F X 2 . -999.99 100 48 0 062312 * . G F X 2 . -999.99 105 48 0 062312 * . G F X 2 . -999.99 110 50 0 062412 * . G F X 2 . -999.99 110 46 0 062412 * . G F X 2 . -999.99 110 50 0 062412 * . G F X 2 . -999.99 115 50 0 062412 * . G F X 2 . -999.99 100 50 0 062412 * . G F X 2 . -999.99 100 50 0 062512 * . G F X 2 . -999.99 98 48 0 062512 * . G F X 2 . -999.99 98 48 0 062512 * . G F X 2 . -999.99 110 48 0 062512 * . G F X 2 . -999.99 110 48 0 062512 * . G F X 2 . -999.99 100 50 0 062512 * . G F X 2 . -999.99 110 48 0 062612 * . G F X 2 . -999.99 100 48 0 062612 * . G F X 2 . -999.99 110 50 0 062612 * . G F X 2 . -999.99 110 50 0 062612 * . G F X 2 . -999.99 100 46 0 062612 * . G F X 2 . -999.99 105 50 0 062612 * . G F. X 2 . -999.99 105 50 0 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 062512 * . G . F X 2 . -999.99 0 062512 * . G F . X 2 . -999.99 0 062512 * . G F . X 2 . -999.99 0 062512 * . G . F X 2 . -999.99 0 062612 * . G F . X 2 . -999.99 0 062612 * . G F X 2 . -999.99 0 062612 * . G F . X 2 . -999.99 0 062612 * . G F . X 2 . -999.99 0 062612 * . G F . X 2 . -999.99 0 062612 * . G F . X 2 . -999.99 0

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Page 40: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 062712-070312_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 07/06/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 07/06/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 060112C * . G . F X 2 . -999.99 -5 -5 0 062712 * . G F. X 2 . -999.99 105 50 0 062712 * . G F . X 2 . -999.99 110 48 0 062812 * . G F . X 2 . -999.99 110 48 0 062812 * . G F . X 2 . -999.99 110 49 0 062912 * . G F . X 2 . -999.99 100 42 1 062912 * . G F . X 2 . -999.99 98 44 0 062912 * . G F . X 2 . -999.99 110 48 0 062912 * . G F. X 2 . -999.99 103 50 0 062912 * . G F. X 2 . -999.99 105 50 0 062912 * . G F . X 2 . -999.99 98 46 0 063012 * . G F. X 2 . -999.99 102 46 0 063012 * . G F . X 2 . -999.99 110 48 0 063012 * . G F . X 2 . -999.99 110 50 0 063012 * . G F . X 2 . -999.99 110 48 0 063012 * . G F . X 2 . -999.99 102 47 0 063012 * . G F . X 2 . -999.99 104 45 0 063012 * . G F . X 2 . -999.99 110 48 0 070112 * . G F . X 2 . -999.99 105 45 0 070112 * . G F . X 2 . -999.99 110 48 0 070112 * . G F. X 2 . -999.99 110 47 0 070112 * . G F. X 2 . -999.99 105 48 0 070212 * . G F. X 2 . -999.99 120 50 1 070212 * . G F. X 2 . -999.99 120 50 0 070212 * . G F. X 2 . -999.99 105 46 0 070212 * . G F. X 2 . -999.99 105 48 0 070212 * . G F X 2 . -999.99 100 48 1 070212 * . G F. X 2 . -999.99 100 48 0 070312 * . G F. X 2 . -999.99 100 48 0 070312 * . G F. X 2 . -999.99 102 48 0 070312 * . G F. X 2 . -999.99 105 48 0 070312 * . G F. X 2 . -999.99 106 48 0 070312 * . G F. X 2 . -999.99 120 48 0 070312 * . G F. X 2 . -999.99 120 48 0 070312 * . G F. X 2 . -999.99 120 50 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 070212 * . G F . X 2 . -999.99 0 070212 * . G F X 2 . -999.99 1 070212 * . G F . X 2 . -999.99 0 070312 * . G F . X 2 . -999.99 0 070312 * . G F . X 2 . -999.99 0 070312 * . G F X 2 . -999.99 0 070312 * . G F . X 2 . -999.99 0 070312 * . G F . X 2 . -999.99 0 070312 * . G F X 2 . -999.99 0 070312 * . G F . X 2 . -999.99 0

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Page 41: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 070412-071112_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 07/17/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 07/17/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 060112C * . G . F X 2 . -999.99 -5 -5 0 070112C * . G F . X 2 . -999.99 -5 -5 0 070412 * . G F. X 2 . -999.99 105 48 0 070512 * . G F . X 2 . -999.99 120 50 1 070512 * . G F . X 2 . -999.99 120 50 0 070512 * . G F . X 2 . -999.99 120 48 1 070512 * . G F . X 2 . -999.99 102 50 0 070512 * . G F . X 2 . -999.99 110 48 1 070512 * . G F . X 2 . -999.99 110 48 1 070612 * . G F . X 2 . -999.99 110 48 0 070612 * . G F . X 2 . -999.99 110 48 0 070612 * . G F . X 2 . -999.99 99 46 0 070612 * . G F . X 2 . -999.99 102 46 0 070612 * . G F . X 2 . -999.99 110 50 0 070712 * . G F . X 2 . -999.99 110 50 0 070712 * . G F . X 2 . -999.99 105 48 1 070712 * . G F . X 2 . -999.99 105 48 0 070712 * . G F . X 2 . -999.99 105 50 0 070812 * . G F . X 2 . -999.99 110 49 0 070812 * . G F . X 2 . -999.99 110 50 0 070812 * . G F . X 2 . -999.99 110 48 0 070812 * . G F . X 2 . -999.99 110 48 0 070812 * . G F . X 2 . -999.99 120 50 0 070912 * . G F . X 2 . -999.99 105 50 0 070912 * . G F . X 2 . -999.99 99 48 1 071012 * . G F . X 2 . -999.99 110 45 0 071012 * . G F . X 2 . -999.99 100 50 0 071012 * . G F . X 2 . -999.99 100 47 0 071012 * . G F . X 2 . -999.99 110 48 0 071112 * . G F . X 2 . -999.99 100 47 0 071112 * . G F . X 2 . -999.99 100 47 0 071112 * . G F . X 2 . -999.99 100 48 0 071112 * . G F . X 2 . -999.99 100 47 0 071112 * . G F . X 2 . -999.99 110 48 0 071112 * . G F . X 2 . -999.99 110 48 0 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 071012 * . G .F X 2 . -999.99 0 071012 * . G F . X 2 . -999.99 0 071012 * . G F . X 2 . -999.99 0 071012 * . G F . X 2 . -999.99 0 071112 * . G F . X 2 . -999.99 0 071112 * . G F . X 2 . -999.99 0 071112 * . G F . X 2 . -999.99 0 071112 * . G F X 2 . -999.99 0 071112 * . G F . X 2 . -999.99 0 071112 * . G F . X 2 . -999.99 0

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Page 42: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 071212-072012_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 07/24/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 07/24/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 060112C * . G . F X 2 . -999.99 -5 -5 0 070112C * . G F . X 2 . -999.99 -5 -5 0 071212 * . G F . X 2 . -999.99 100 48 1 071212 * . G F . X 2 . -999.99 105 50 0 071212 * . G F . X 2 . -999.99 105 50 0 071212 * . G F . X 2 . -999.99 125 50 1 071312 * . G F . X 2 . -999.99 102 50 1 071312 * . G F . X 2 . -999.99 105 48 0 071312 * . G F . X 2 . -999.99 105 47 0 071412 * . G F . X 2 . -999.99 99 48 0 071412 * . G F . X 2 . -999.99 110 50 0 071412 * . G F . X 2 . -999.99 100 48 0 071512 * . G F . X 2 . -999.99 101 45 0 071512 * . G F . X 2 . -999.99 110 50 0 071512 * . G F . X 2 . -999.99 100 48 0 071512 * . G F. X 2 . -999.99 110 48 0 071512 * . G F. X 2 . -999.99 110 48 0 071612 * . G F. X 2 . -999.99 105 48 0 071612 * . G F. X 2 . -999.99 105 45 0 071712 * . G F. X 2 . -999.99 100 50 0 071712 * . G F. X 2 . -999.99 100 48 0 071712 * . G F. X 2 . -999.99 120 48 0 071812 * . G F. X 2 . -999.99 102 45 0 071812 * . G F. X 2 . -999.99 110 50 0 071812 * . G F. X 2 . -999.99 110 50 0 071812 * . G F . X 2 . -999.99 105 48 0 071912 * . G F . X 2 . -999.99 105 48 0 071912 * . G F. X 2 . -999.99 110 50 0 071912 * . G F . X 2 . -999.99 100 50 0 071912 * . G F . X 2 . -999.99 100 48 0 071912 * . G F . X 2 . -999.99 100 48 0 071912 * . G F . X 2 . -999.99 110 48 0 072012 * . G F . X 2 . -999.99 90 48 0 072012 * . G F . X 2 . -999.99 100 50 0 072012 * . G F . X 2 . -999.99 105 48 0 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 071812 * . G F . X 2 . -999.99 0 071912 * . G F. X 2 . -999.99 0 071912 * . G F X 2 . -999.99 0 071912 * . G F . X 2 . -999.99 0 071912 * . G F . X 2 . -999.99 0 071912 * . G F . X 2 . -999.99 0 071912 * . G F . X 2 . -999.99 0 072012 * . G F . X 2 . -999.99 0 072012 * . G F . X 2 . -999.99 0 072012 * . G F X 2 . -999.99 0

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Page 43: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 072412-073112_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 08/01/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 08/01/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 060112C * . G . F X 2 . -999.99 -5 -5 0 070112C * . G F . X 2 . -999.99 -5 -5 0 072412 * . G F X 2 . -999.99 105 48 0 072512 * . G F X 2 . -999.99 100 48 0 072512 * . G F X 2 . -999.99 100 48 0 072512 * . G F X 2 . -999.99 110 48 0 072612 * . G F X 2 . -999.99 100 48 0 072612 * . G F X 2 . -999.99 100 43 0 072612 * . G F. X 2 . -999.99 120 42 0 072612 * . G F. X 2 . -999.99 110 48 0 072612 * . G F . X 2 . -999.99 110 47 0 072712 * . G F . X 2 . -999.99 100 48 0 072712 * . G F . X 2 . -999.99 100 48 0 072712 * . G F . X 2 . -999.99 110 48 0 072712 * . G F . X 2 . -999.99 110 50 0 072712 * . G F . X 2 . -999.99 110 50 0 072712 * . G F . X 2 . -999.99 105 45 0 072812 * . G F . X 2 . -999.99 95 48 0 072812 * . G F . X 2 . -999.99 110 50 0 072812 * . G F . X 2 . -999.99 102 48 0 072812 * . G F . X 2 . -999.99 100 43 2 072912 * . G F . X 2 . -999.99 105 47 1 072912 * . G F . X 2 . -999.99 105 48 1 072912 * . G F . X 2 . -999.99 105 47 1 072912 * . G F . X 2 . -999.99 105 50 1 072912 * . G F . X 2 . -999.99 110 46 1 072912 * . G F . X 2 . -999.99 110 46 1 072912 * . G F . X 2 . -999.99 110 48 0 073012 * . G F . X 2 . -999.99 100 47 1 073012 * . G F . X 2 . -999.99 100 47 0 073012 * . G F . X 2 . -999.99 110 46 1 073012 * . G F . X 2 . -999.99 110 46 1 073012 * . G F . X 2 . -999.99 110 46 0 073112 * . G F . X 2 . -999.99 110 48 0 073112 * . G F . X 2 . -999.99 110 50 0 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 072912 * . G F . X 2 . -999.99 1 072912 * . G F . X 2 . -999.99 1 072912 * . G F . X 2 . -999.99 0 073012 * . G F . X 2 . -999.99 1 073012 * . G F . X 2 . -999.99 0 073012 * . G F . X 2 . -999.99 1 073012 * . G F X 2 . -999.99 1 073012 * . G F . X 2 . -999.99 0 073112 * . G F . X 2 . -999.99 0 073112 * . G F . X 2 . -999.99 0

Page 1

Page 44: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 080112-080712_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 08/10/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 08/10/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 060112C * . G . F X 2 . -999.99 -5 -5 0 070112C * . G F . X 2 . -999.99 -5 -5 0 080112 * . G F . X 2 . -999.99 97 48 0 080112 * . G F . X 2 . -999.99 110 48 0 080112 * . G F . X 2 . -999.99 100 48 0 080112 * . G F . X 2 . -999.99 105 48 0 080112 * . G F . X 2 . -999.99 110 48 0 080112 * . G F . X 2 . -999.99 105 50 0 080212 * . G F . X 2 . -999.99 105 40 1 080212 * . G F . X 2 . -999.99 110 45 0 080212 * . G F . X 2 . -999.99 105 50 0 080312 * . G F . X 2 . -999.99 100 48 0 080312 * . G F . X 2 . -999.99 100 48 0 080312 * . G F . X 2 . -999.99 105 48 0 080312 * . G F . X 2 . -999.99 95 48 0 080412 * . G F . X 2 . -999.99 100 47 1 080412 * . G F . X 2 . -999.99 95 48 0 080412 * . G F . X 2 . -999.99 95 48 0 080412 * . G F . X 2 . -999.99 100 48 0 080512 * . G F . X 2 . -999.99 105 46 0 080512 * . G F . X 2 . -999.99 110 47 0 080512 * . G F . X 2 . -999.99 110 47 0 080512 * . G F . X 2 . -999.99 98 46 0 080612 * . G F . X 2 . -999.99 105 48 0 080612 * . G F . X 2 . -999.99 105 48 0 080612 * . G F . X 2 . -999.99 110 50 0 080612 * . G F . X 2 . -999.99 100 48 0 080612 * . G F . X 2 . -999.99 105 47 0 080712 * . G F . X 2 . -999.99 102 49 0 080712 * . G F . X 2 . -999.99 98 45 0 080712 * . G F . X 2 . -999.99 102 48 0 080712 * . G F . X 2 . -999.99 100 48 0 080712 * . G F . X 2 . -999.99 105 48 0 080712 * . G F . X 2 . -999.99 100 48 0 080712 * . G F . X 2 . -999.99 95 48 0 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 080612 * . G F . X 2 . -999.99 0 080612 * . G . F X 2 . -999.99 0 080612 * . G F. X 2 . -999.99 0 080712 * . G .F X 2 . -999.99 0 080712 * . G F X 2 . -999.99 0 080712 * . G F X 2 . -999.99 0 080712 * . G F X 2 . -999.99 0 080712 * . G F . X 2 . -999.99 0 080712 * . G .F X 2 . -999.99 0 080712 * . G F. X 2 . -999.99 0

Page 1

Page 45: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 080812-081712_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 08/22/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 08/22/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 060112C * . G . F X 2 . -999.99 -5 -5 0 070112C * . G F . X 2 . -999.99 -5 -5 0 080112C * . G F . X 2 . -999.99 -5 -5 0 080812 * . G F . X 2 . -999.99 95 42 0 080912 * . G F . X 2 . -999.99 100 46 0 080912 * . G F . X 2 . -999.99 100 48 0 080912 * . G F . X 2 . -999.99 100 48 0 080912 * . G F . X 2 . -999.99 105 45 0 081012 * . G F . X 2 . -999.99 95 48 0 081012 * . G F . X 2 . -999.99 105 50 0 081012 * . G F . X 2 . -999.99 105 50 0 081012 * . G F . X 2 . -999.99 105 48 0 081112 * . G F . X 2 . -999.99 110 46 0 081112 * . G F . X 2 . -999.99 110 50 0 081112 * . G F . X 2 . -999.99 120 50 0 081212 * . G F . X 2 . -999.99 110 47 0 081212 * . G F . X 2 . -999.99 110 49 0 081212 * . G F . X 2 . -999.99 110 48 0 081212 * . G F . X 2 . -999.99 120 48 0 081312 * . G F . X 2 . -999.99 107 50 0 081312 * . G F . X 2 . -999.99 105 48 0 081312 * . G F . X 2 . -999.99 120 45 0 081312 * . G F . X 2 . -999.99 120 45 0 081412 * . G F . X 2 . -999.99 105 50 0 081412 * . G F . X 2 . -999.99 110 50 0 081412 * . G F . X 2 . -999.99 110 50 0 081512 * . G F . X 2 . -999.99 110 50 0 081512 * . G F . X 2 . -999.99 105 47 0 081512 * . G F . X 2 . -999.99 110 48 0 081612 * . G F . X 2 . -999.99 120 50 0 081612 * . G F . X 2 . -999.99 110 50 0 081712 * . G F . X 2 . -999.99 105 48 0 081712 * . G F . X 2 . -999.99 100 47 0 081712 * . G F . X 2 . -999.99 100 43 1 081712 * . G F . X 2 . -999.99 100 48 0 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 081412 * . G F . X 2 . -999.99 0 081512 * . G F. X 2 . -999.99 0 081512 * . G F. X 2 . -999.99 0 081512 * . G F . X 2 . -999.99 0 081612 * . G F . X 2 . -999.99 0 081612 * . G F . X 2 . -999.99 0 081712 * . G . F X 2 . -999.99 0 081712 * . G F . X 2 . -999.99 0 081712 * . G . +F X 2 . -999.99 1 081712 * . G F . X 2 . -999.99 0

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Page 46: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 081812-082512_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 08/28/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 08/28/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 060112C * . G . F X 2 . -999.99 -5 -5 0 070112C * . G F . X 2 . -999.99 -5 -5 0 080112C * . G F . X 2 . -999.99 -5 -5 0 081912 * . G F X 2 . -999.99 110 50 1 081912 * . G .F X 2 . -999.99 110 50 1 081912 * . G .F X 2 . -999.99 100 48 0 082012 * . G .F X 2 . -999.99 100 46 0 082012 * . G .F X 2 . -999.99 100 48 0 082012 * . G .F X 2 . -999.99 105 48 0 082012 * . G .F X 2 . -999.99 105 47 0 082012 * . G .F X 2 . -999.99 110 48 0 082112 * . G .F X 2 . -999.99 100 50 0 082112 * . G .F X 2 . -999.99 100 50 0 082112 * . G .F X 2 . -999.99 110 48 0 082112 * . G .F X 2 . -999.99 110 47 0 082212 * . G .F X 2 . -999.99 90 48 0 082212 * . G .F X 2 . -999.99 110 50 0 082212 * . G .F X 2 . -999.99 110 50 1 082212 * . G .F X 2 . -999.99 110 50 0 082212 * . G .F X 2 . -999.99 110 48 0 082312 * . G .F X 2 . -999.99 110 48 0 082312 * . G F X 2 . -999.99 110 45 0 082312 * . G F X 2 . -999.99 120 48 0 082312 * . G F X 2 . -999.99 105 45 0 082312 * . G F X 2 . -999.99 110 48 0 082412 * . G F X 2 . -999.99 109 50 0 082412 * . G F. X 2 . -999.99 104 50 0 082412 * . G F. X 2 . -999.99 110 50 0 082412 * . G F. X 2 . -999.99 110 50 0 082412 * . G F. X 2 . -999.99 110 45 0 082412 * . G F. X 2 . -999.99 110 48 0 082412 * . G F. X 2 . -999.99 100 48 0 082512 * . G F. X 2 . -999.99 120 50 0 082512 * . G F. X 2 . -999.99 120 50 0 082512 * . G F. X 2 . -999.99 105 48 1 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 082412 * . G F . X 2 . -999.99 0 082412 * . G F . X 2 . -999.99 0 082412 * . G .F X 2 . -999.99 0 082412 * . G F . X 2 . -999.99 0 082412 * . G F . X 2 . -999.99 0 082412 * . G F . X 2 . -999.99 0 082412 * . G F. X 2 . -999.99 0 082512 * . G F . X 2 . -999.99 0 082512 * . G F. X 2 . -999.99 0 082512 * . G F. X 2 . -999.99 1

Page 1

Page 47: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 082612-090312_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 09/14/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 09/14/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * . G . F X 2 . -999.99 -5 -5 0 060112C * . G . F X 2 . -999.99 -5 -5 0 070112C * . G F . X 2 . -999.99 -5 -5 0 080112C * . G F . X 2 . -999.99 -5 -5 0 082712 * . G F X 2 . -999.99 100 50 0 082712 * . G F X 2 . -999.99 110 50 0 082712 * . G F X 2 . -999.99 120 50 0 082712 * . G F X 2 . -999.99 120 50 0 082712 * . G F. X 2 . -999.99 100 46 0 082712 * . G F. X 2 . -999.99 100 47 0 082812 * . G F. X 2 . -999.99 105 47 0 082812 * . G F . X 2 . -999.99 98 48 0 082912 * . G F. X 2 . -999.99 100 45 0 082912 * . G F . X 2 . -999.99 100 45 0 082912 * . G F . X 2 . -999.99 100 48 0 082912 * . G F . X 2 . -999.99 100 43 0 082912 * . G F . X 2 . -999.99 110 48 0 082912 * . G F . X 2 . -999.99 100 48 0 082912 * . G F . X 2 . -999.99 110 45 0 083012 * . G F . X 2 . -999.99 110 48 0 083012 * . G F . X 2 . -999.99 102 48 0 083012 * . G F . X 2 . -999.99 110 48 0 083012 * . G F . X 2 . -999.99 100 48 0 083012 * . G F . X 2 . -999.99 110 48 0 083112 * . G F . X 2 . -999.99 100 47 0 083112 * . G F . X 2 . -999.99 120 48 0 083112 * . G F . X 2 . -999.99 120 48 0 083112 * . G F . X 2 . -999.99 105 46 0 090112 * . G F . X 2 . -999.99 105 48 0 090112 * . G F . X 2 . -999.99 105 48 0 090212 * . G F . X 2 . -999.99 115 47 0 090312 * . G F . X 2 . -999.99 110 50 0 090312 * . G F . X 2 . -999.99 110 48 0 090312 * . G F . X 2 . -999.99 110 48 1 090312 * . G F . X 2 . -999.99 110 45 0 090312 * . G F . X 2 . -999.99 100 48 0 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -8...-6...-4...F/F...0....2....4 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 083112 * . G F. X 2 . -999.99 0 083112 * . G F . X 2 . -999.99 0 090112 * . G .F X 2 . -999.99 0 090112 * . G F . X 2 . -999.99 0 090212 * . G F . X 2 . -999.99 0 090312 * . G F . X 2 . -999.99 0 090312 * . G F. X 2 . -999.99 0 090312 * . G F . X 2 . -999.99 1 090312 * . G F . X 2 . -999.99 0 090312 * . G F . X 2 . -999.99 0

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Page 48: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 090112-091012_PK-YTU_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 09/14/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 09/14/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTU -1 B737-300 CFM56-3C-1 722283 120410 0 1 20.0 VARIED) 10...20...30...EGT..50...60...70 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 041712A V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 041712B V=-999.0 R=-999.0 7.5 2.85 N2=-1.78 VSV=-999.00 -999.99 -5 -5 0 050112C * G . F X 2 . -999.99 -5 -5 0 060112C * . G . F X 2 . -999.99 -5 -5 0 070112C * . G F . X 2 . -999.99 -5 -5 0 080112C * . G F . X 2 . -999.99 -5 -5 0 090112 * . G F . X 2 . -999.99 105 48 0 090112 * . G F . X 2 . -999.99 105 48 0 090212 * . G F . X 2 . -999.99 115 47 0 090312 * . G F . X 2 . -999.99 110 50 0 090312 * . G F . X 2 . -999.99 110 48 0 090312 * . G F . X 2 . -999.99 110 48 1 090312 * . G F . X 2 . -999.99 110 45 0 090312 * . G F . X 2 . -999.99 100 48 0 090412 * . G F . X 2 . -999.99 102 50 0 090412 * . G F . X 2 . -999.99 105 48 0 090412 * . G F . X 2 . -999.99 98 47 0 090412 * . G F . X 2 . -999.99 110 48 0 090412 * . G F . X 2 . -999.99 110 48 0 090512 * . G F . X 2 . -999.99 101 48 0 090512 * . G F . X 2 . -999.99 105 48 0 090512 * . G F . X 2 . -999.99 105 48 0 090512 * . G F . X 2 . -999.99 105 49 0 090612 * . G F . X 2 . -999.99 120 47 0 090612 * . G F . X 2 . -999.99 105 46 0 090612 * . G F . X 2 . -999.99 105 48 0 090612 * . G F . X 2 . -999.99 105 42 0 090712 * . G F . X 2 . -999.99 99 48 0 090712 * . G F . X 2 . -999.99 105 46 0 090712 * . G F . X 2 . -999.99 110 47 0 090812 * . G F . X 2 . -999.99 100 48 1 090812 * . G F . X 2 . -999.99 100 48 2 090812 * . G F. X 2 . -999.99 100 48 1 090912 * . G F . X 2 . -999.99 120 50 0 090912 * . G F . X 2 . -999.99 105 50 0 090912 * . G F . X 2 . -999.99 110 50 0 090912 * . G F . X 2 . -999.99 110 48 0 091012 * . G F . X 2 . -999.99 100 48 0 RAW DATA 10...20...30...EGT..50...60...70 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 -6...-4...-2...F/F...2....4....6 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 090712 * . G F. X 2 . -999.99 0 090712 * . G F . X 2 . -999.99 0 090812 * . G .F X 2 . -999.99 1 090812 * . G . F X 2 . -999.99 2 090812 * . G . F X 2 . -999.99 1 090912 * . G F . X 2 . -999.99 0 090912 * . G F . X 2 . -999.99 0 090912 * . G F . X 2 . -999.99 0 090912 * . G F . X 2 . -999.99 0 091012 * . G F . X 2 . -999.99 0

Page 1

Page 49: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 112312-110412_PK-YTE_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 12/07/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 12/07/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTE -1 B737-400 CFM56-3C-1 722283 121004 0 1 22.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 72...74...76...F/F..80...82...84 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 112512A V=-999.0 R=-999.0 28.4 118.16 N2=-1.01 VSV=-999.00 -999.99 -5 -5 0 112512B V=-999.0 R=-999.0 28.4 118.16 N2=-1.01 VSV=-999.00 -999.99 -5 -5 0 112312 * X X X X -999.99 110 48 0 112312 * X X X X -999.99 110 45 0 112412 * X X X X -999.99 110 50 0 112412 * X X X X -999.99 110 50 0 112412 * X X X X -999.99 102 48 0 112412 * X X X X -999.99 105 49 0 112512 * X X X X -999.99 110 47 0 112512 * X X X X -999.99 110 50 0 112512 * X X X X -999.99 110 48 0 112512 * . G . +F X 2 . -999.99 110 48 0 112612 * . G . +F X 2 . -999.99 100 48 0 112612 * . G . +F X 2 . -999.99 100 48 0 112712 * . G . +F X 2 . -999.99 105 48 0 112712 * . G . +F X 2 . -999.99 110 48 0 112812 * . G . +F X 2 . -999.99 100 48 0 112812 * . G . +F X 2 . -999.99 100 48 0 112812 * . G . +F X 2 . -999.99 110 48 0 112812 * . G . +F X 2 . -999.99 110 48 0 112812 * . G . +F X 2 . -999.99 100 50 0 112912 * . G . +F X 2 . -999.99 102 51 0 112912 * . G . +F X 2 . -999.99 105 48 0 113012 * . G . +F X 2 . -999.99 105 50 0 113012 * . G . +F X 2 . -999.99 100 48 0 113012 * . G . +F X 2 . -999.99 100 48 0 113012 * . G . +F X 2 . -999.99 98 48 0 113012 * . G . +F X 2 . -999.99 110 50 0 120112 * . G . +F X 2 . -999.99 105 50 0 120112 * . G . +F X 2 . -999.99 110 48 0 120112 * . G . +F X 2 . -999.99 110 49 0 120112 * . G . +F X 2 . -999.99 110 48 0 120212 * . G . +F X 2 . -999.99 102 50 0 120212 * . G . F X 2 . -999.99 120 49 0 120212 * . G -F X 2 . -999.99 110 48 0 120212 * . G -F X 2 . -999.99 110 50 0 120312 * . G -F X 2 . -999.99 110 50 0 120412 * . G -F X 2 . -999.99 101 48 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 72...74...76...F/F..80...82...84 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 120112 * . G -F X 2 . -999.99 0 120112 * . G -F X 2 . -999.99 0 120112 * . G . +F X 2 . -999.99 0 120112 * . -FG X 2 . -999.99 0 120212 * . G -F X 2 . -999.99 0 120212 * . G -F X 2 . -999.99 0 120212 * . G -F X 2 . -999.99 0 120212 * . G-F X 2 . -999.99 0 120312 * . G . +F X 2 . -999.99 0 120412 * . G-F X 2 . -999.99 0

Page 1

Page 50: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 120512-121612_PK-YTE_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 12/17/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 12/17/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTE -1 B737-400 CFM56-3C-1 722283 121004 0 1 22.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 108..110..112...F/F.116..118..120 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 112512A V=-999.0 R=-999.0 28.4 118.16 N2=-1.01 VSV=-999.00 -999.99 -5 -5 0 112512B V=-999.0 R=-999.0 28.4 118.16 N2=-1.01 VSV=-999.00 -999.99 -5 -5 0 120212 * . G -F X 2 . -999.99 110 50 0 120312 * . G -F X 2 . -999.99 110 50 0 120412 * . G -F X 2 . -999.99 101 48 0 120512 * . G -F X 2 . -999.99 110 48 1 120512 * . G -F X 2 . -999.99 100 48 1 120512 * . G -F X 2 . -999.99 105 48 1 120612 * . G -F X 2 . -999.99 110 48 1 120612 * . G -F X 2 . -999.99 100 48 1 120612 * . G -F X 2 . -999.99 100 47 1 120712 * . G -F X 2 . -999.99 110 50 1 120712 * . G -F X 2 . -999.99 100 48 1 120712 * . G -F X 2 . -999.99 100 48 1 120712 * . G -F X 2 . -999.99 100 48 1 120712 * . G -F X 2 . -999.99 100 50 1 120912 * . G -F X 2 . -999.99 110 50 1 120912 * . G -F X 2 . -999.99 100 48 1 121012 * . G -F X 2 . -999.99 105 48 1 121012 * . G -F X 2 . -999.99 105 50 2 121012 * . G -F X 2 . -999.99 110 50 1 121012 * . G -F X 2 . -999.99 100 48 2 121012 * . G -F X 2 . -999.99 102 40 2 121112 * . G F X 2 . -999.99 100 48 1 121112 * . G . F X 2 . -999.99 110 48 1 121212 * . G . F X 2 . -999.99 110 50 1 121212 * . G . F X 2 . -999.99 110 54 2 121312 * . G . F X 2 . -999.99 100 50 1 121412 * . G . F X 2 . -999.99 110 48 1 121412 * . G . F X 2 . -999.99 90 47 1 121412 * . G . F X 2 . -999.99 110 48 1 121512 * . G . F X 2 . -999.99 110 48 1 121512 * . G . F X 2 . -999.99 105 48 1 121512 * . G . F X 2 . -999.99 105 48 1 121612 * . G . F X 2 . -999.99 102 48 1 121612 * . G . F X 2 . -999.99 100 49 1 121612 * . G . F X 2 . -999.99 100 48 0 121612 * . G . F X 2 . -999.99 100 48 0 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 108..110..112...F/F.116..118..120 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 121412 * . G . F X 2 . -999.99 1 121412 * . G . F X 2 . -999.99 1 121412 * . G . F X 2 . -999.99 1 121512 * . G . F X 2 . -999.99 1 121512 * . G . F X 2 . -999.99 1 121512 * . G . F X 2 . -999.99 1 121612 * . G . F X 2 . -999.99 1 121612 * . G . +F2 X . -999.99 1 121612 * . G . F X 2 . -999.99 0 121612 * . G . F X 2 . -999.99 0

Page 1

Page 51: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 121712-122612_PK-YTE_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 12/27/2012 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 12/27/2012 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTE -1 B737-400 CFM56-3C-1 722283 121004 0 1 22.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 112..114..116...F/F.120..122..124 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 112512A V=-999.0 R=-999.0 28.4 118.16 N2=-1.01 VSV=-999.00 -999.99 -5 -5 0 112512B V=-999.0 R=-999.0 28.4 118.16 N2=-1.01 VSV=-999.00 -999.99 -5 -5 0 112612C * . G . F X 2 . -999.99 -5 -5 0 120112C * . G -F X 2 . -999.99 -5 -5 0 121612 * . G . F X 2 . -999.99 100 48 0 121712 * . G . F X 2 . -999.99 105 48 0 121712 * . G . F X 2 . -999.99 105 48 0 121712 * . G . F X 2 . -999.99 110 48 0 121812 * . G . F X 2 . -999.99 105 56 1 121812 * . G . F X 2 . -999.99 105 50 0 121812 * . G . F X 2 . -999.99 105 50 0 121912 * . G . F X 2 . -999.99 105 49 0 121912 * . G . F X 2 . -999.99 100 49 0 121912 * . G . F X 2 . -999.99 100 48 0 121912 * . G . F X 2 . -999.99 110 49 0 121912 * . G . F X 2 . -999.99 100 49 0 122012 * . G . F X 2 . -999.99 100 48 0 122012 * . G . F X 2 . -999.99 100 48 0 122012 * . G . F X 2 . -999.99 100 48 0 122012 * . G . F X 2 . -999.99 104 48 0 122112 * . G . F X 2 . -999.99 102 48 0 122112 * . G . F X 2 . -999.99 100 48 0 122112 * . G . F X 2 . -999.99 100 48 0 122212 * . G . F X 2 . -999.99 100 48 0 122212 * . G . F X 2 . -999.99 105 48 0 122212 * . G . F X 2 . -999.99 110 50 2 122212 * . G . F X 2 . -999.99 110 48 0 122312 * . G . F X 2 . -999.99 100 48 0 122312 * . G . F X 2 . -999.99 100 50 0 122312 * . G . F X 2 . -999.99 110 50 0 122412 * . G . F X 2 . -999.99 110 50 1 122512 * . G . F X 2 . -999.99 100 48 0 122512 * . G . F X 2 . -999.99 99 48 0 122612 * . G . F X 2 . -999.99 100 48 0 122612 * . G . F X 2 . -999.99 100 48 1 122612 * . G . F X 2 . -999.99 99 48 1 122612 * . G . F X 2 . -999.99 110 47 0 122612 * . G . F X 2 . -999.99 105 50 0 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 112..114..116...F/F.120..122..124 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 122312 * . G . F X 2 . -999.99 0 122312 * . G . F X 2 . -999.99 0 122412 * . G . +F X 2 . -999.99 1 122512 * . G . F X 2 . -999.99 0 122512 * . G . F X 2 . -999.99 0 122612 * . G . F X 2 . -999.99 0 122612 * . G . F X 2 . -999.99 1 122612 * . G . F X 2 . -999.99 1 122612 * . G . F X 2 . -999.99 0 122612 * . G . F X 2 . -999.99 0

Page 1

Page 52: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 122712-010513_PK-YTE_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 01/07/2013 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 01/07/2013 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTE -1 B737-400 CFM56-3C-1 722283 121004 0 1 22.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 112..114..116...F/F.120..122..124 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 112512A V=-999.0 R=-999.0 28.4 118.16 N2=-1.01 VSV=-999.00 -999.99 -5 -5 0 112512B V=-999.0 R=-999.0 28.4 118.16 N2=-1.01 VSV=-999.00 -999.99 -5 -5 0 112612C * . G . F X 2 . -999.99 -5 -5 0 120112C * . G -F X 2 . -999.99 -5 -5 0 122712 * . G . F X 2 . -999.99 110 50 0 122712 * . G . F X 2 . -999.99 110 48 0 122712 * . G . F X 2 . -999.99 110 48 0 122712 * . G . F X 2 . -999.99 100 48 0 122712 * . G . F X 2 . -999.99 110 52 0 122812 * . G . F X 2 . -999.99 100 47 0 122812 * . G . F X 2 . -999.99 102 49 0 122812 * . G . F X 2 . -999.99 105 50 0 122912 * . G . F X 2 . -999.99 110 48 0 122912 * . G . F X 2 . -999.99 100 48 0 122912 * . G . F X 2 . -999.99 98 48 0 123012 * . G . F X 2 . -999.99 110 48 0 123012 * . G . F X 2 . -999.99 100 48 0 123112 * . G . F X 2 . -999.99 100 48 0 123112 * . G . F X 2 . -999.99 100 48 0 010113 * . G . F X 2 . -999.99 105 47 0 010113 * . G . F X 2 . -999.99 107 48 0 010213 * . G . F X 2 . -999.99 105 48 0 010213 * . G . F X 2 . -999.99 100 48 0 010213 * . G . F X 2 . -999.99 110 48 0 010213 * . G . F X 2 . -999.99 102 48 0 010213 * . G . F X 2 . -999.99 98 47 0 010313 * . G . F X 2 . -999.99 101 50 0 010313 * . G . F X 2 . -999.99 100 50 0 010313 * . G . F X 2 . -999.99 105 50 1 010413 * . G . F X 2 . -999.99 95 47 0 010413 * . G . F X 2 . -999.99 110 48 0 010413 * . G . F X 2 . -999.99 100 48 0 010413 * . G . F X 2 . -999.99 100 48 0 010413 * . G . F X 2 . -999.99 105 47 0 010513 * . G . F X 2 . -999.99 100 45 0 010513 * . G . F X 2 . -999.99 110 48 0 010513 * . G . F X 2 . -999.99 100 48 0 010513 * . G . F X 2 . -999.99 100 48 0 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 112..114..116...F/F.120..122..124 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 010313 * . G . F X 2 . -999.99 1 010413 * . G . F X 2 . -999.99 0 010413 * . G . F X 2 . -999.99 0 010413 * . G . F X 2 . -999.99 0 010413 * . G . F X 2 . -999.99 0 010413 * . G . F X 2 . -999.99 0 010513 * . G . F X 2 . -999.99 0 010513 * . G . F X 2 . -999.99 0 010513 * . G . F X 2 . -999.99 0 010513 * . G . F X 2 . -999.99 0

Page 1

Page 53: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 010613-011513_PK-YTE_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 01/16/2013 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 01/16/2013 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTE -1 B737-400 CFM56-3C-1 722283 121004 0 1 22.0 VARIED) -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 112..114..116...F/F.120..122..124 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 112512A V=-999.0 R=-999.0 28.4 118.16 N2=-1.01 VSV=-999.00 -999.99 -5 -5 0 112512B V=-999.0 R=-999.0 28.4 118.16 N2=-1.01 VSV=-999.00 -999.99 -5 -5 0 112612C * . G . F X 2 . -999.99 -5 -5 0 120112C * . G -F X 2 . -999.99 -5 -5 0 010113C * . G . F X 2 . -999.99 -5 -5 0 010613 * . G . F X 2 . -999.99 100 48 0 010613 * . G . F X 2 . -999.99 100 47 0 010713 * . G . F X 2 . -999.99 103 50 0 010713 * . G . F X 2 . -999.99 100 48 0 010713 * . G . F X 2 . -999.99 110 48 0 010813 * . G . F X 2 . -999.99 110 50 0 010813 * . G . F X 2 . -999.99 105 46 0 010913 * . G . F X 2 . -999.99 110 47 0 010913 * . G . F X 2 . -999.99 100 47 1 010913 * . G . F X 2 . -999.99 100 47 1 010913 * . G . F X 2 . -999.99 98 47 0 011013 * . G . F X 2 . -999.99 102 48 0 011013 * . G . F X 2 . -999.99 98 46 0 011013 * . G . F X 2 . -999.99 100 50 0 011113 * . G . F X 2 . -999.99 100 48 0 011113 * . G . F X 2 . -999.99 110 50 0 011113 * . G . F X 2 . -999.99 105 50 0 011113 * . G . F X 2 . -999.99 110 49 0 011113 * . G . F X 2 . -999.99 95 42 0 011213 * . G . F X 2 . -999.99 100 48 0 011213 * . G . F X 2 . -999.99 105 48 0 011213 * . G . F X 2 . -999.99 100 48 0 011213 * . G . F X 2 . -999.99 110 48 0 011313 * . G . F X 2 . -999.99 95 50 2 011313 * . G . F X 2 . -999.99 105 48 1 011413 * . G . F X 2 . -999.99 105 48 0 011413 * . G . F X 2 . -999.99 105 50 0 011413 * . G . F X 2 . -999.99 105 50 1 011413 * . G . F X 2 . -999.99 105 48 0 011413 * . G . F X 2 . -999.99 100 50 0 011513 * . G . F X 2 . -999.99 110 60 1 011513 * . G . F X 2 . -999.99 100 48 1 011513 * . G . F X 2 . -999.99 100 48 0 RAW DATA -10....0...10...EGT..30...40...50 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 112..114..116...F/F.120..122..124 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 011313 * . G . F X 2 . -999.99 2 011313 * . G . F X 2 . -999.99 1 011413 * . G . F X 2 . -999.99 0 011413 * . G . F X 2 . -999.99 0 011413 * . G . F X 2 . -999.99 1 011413 * . G . F X 2 . -999.99 0 011413 * . G . F X 2 . -999.99 0 011513 * . -F +G -2 X . -999.99 1 011513 * . G . F X 2 . -999.99 1 011513 * . G . F X 2 . -999.99 0

Page 1

Page 54: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

eng1 011613-012413_PK-YTE_1.txt1 REPORT ID: CRTRND GE ENGINE CONDITION MONITORING PROGRAM SAGE V4.1.1 - JUL 2001 REPORT DATE: 01/29/2013 CRUISE PERFORMANCE MONITORING - FROM 01/01/1980 TO 01/29/2013 PAGE: 1 AIRTYP ENGTYP ENGSN INSDAT N1MOD TCC FNRAT CONFIG CONTROL SELECTOR (SCALES PK-YTE -1 B737-400 CFM56-3C-1 722283 121004 0 1 22.0 VARIED) 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 SMOOTH 0....1.VIB2....3 114..116..118...F/F.122..124..126 3....4...VSV...6....7 CRZ OIL OIL MAINT ALT DATE SLOATL TMP PRS CODES CTR 112512A V=-999.0 R=-999.0 28.4 118.16 N2=-1.01 VSV=-999.00 -999.99 -5 -5 0 112512B V=-999.0 R=-999.0 28.4 118.16 N2=-1.01 VSV=-999.00 -999.99 -5 -5 0 112612C * . G . F X 2 . -999.99 -5 -5 0 120112C * . G -F X 2 . -999.99 -5 -5 0 010113C * . G . F X 2 . -999.99 -5 -5 0 011713 * . G . F X 2 . -999.99 98 48 0 011713 * . G . F X 2 . -999.99 100 50 0 011713 * . G . F X 2 . -999.99 120 48 1 011713 * . G . F X 2 . -999.99 120 50 1 011813 * . G . F X 2 . -999.99 120 46 1 011813 * . G . F X 2 . -999.99 105 50 1 011813 * . G . F X 2 . -999.99 100 50 0 011813 * . G . F X 2 . -999.99 105 48 0 011813 * . G . F X 2 . -999.99 105 48 0 011913 * . G . F X 2 . -999.99 120 50 0 011913 * . G . F X 2 . -999.99 105 50 0 012013 * . G . F X 2 . -999.99 100 50 0 012013 * . G . F X 2 . -999.99 105 48 0 012013 * . G . F X 2 . -999.99 95 48 0 012013 * . G . F X 2 . -999.99 105 48 0 012113 * . G . F X 2 . -999.99 100 48 0 012113 * . G . F X 2 . -999.99 100 48 1 012113 * . G . F X 2 . -999.99 100 47 1 012113 * . G . F X 2 . -999.99 100 48 0 012213 * . G . F X 2 . -999.99 101 48 0 012213 * . G . F X 2 . -999.99 120 48 0 012213 * . G . F X 2 . -999.99 100 48 0 012213 * . G . F X 2 . -999.99 100 48 0 012313 * . G . F X 2 . -999.99 105 48 0 012313 * . G . F X 2 . -999.99 100 42 0 012313 * . G . F X 2 . -999.99 95 48 0 012313 * . G . F X 2 . -999.99 100 48 0 012313 * . G . F X 2 . -999.99 105 48 0 012313 * . G . F X 2 . -999.99 105 50 0 012413 * . G . F X 2 . -999.99 98 48 0 012413 * . G . F X 2 . -999.99 100 48 0 012413 * . G . F X 2 . -999.99 110 48 0 012413 * . G . F X 2 . -999.99 100 48 0 RAW DATA 0...10...20...EGT..40...50...60 -3....X...-2....X...N2....X....0....X....1 0....1.VIB2....3 114..116..118...F/F.122..124..126 3....4...VSV...6....7 CRZ MODULE CHG ALT DATE SLOATL MAINT CODES CTR 012313 * . G . F X 2 . -999.99 0 012313 * . G . F X 2 . -999.99 0 012313 * . G . F X 2 . -999.99 0 012313 * . G . F X 2 . -999.99 0 012313 * . G . F X 2 . -999.99 0 012313 * . G . F X 2 . -999.99 0 012413 * . . G F 2 X . -999.99 0 012413 * . G . F X 2 . -999.99 0 012413 * . G . F X 2 . -999.99 0 012413 * . G -F X 2 . -999.99 0

Page 1

Page 55: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 6 of 55

List Of Changed Parts

ESN : 722283 TSN : 58410:95 CSN : 37957

No Disassembly Assembly

Description P/N S/N Remark P/N S/N Remark

1 Fan Blade 1590M21P01 MAE22558-E Repair 1663M24P01 MAA26283 INSPECTED

2 Fan Blade 1663M24P02 MAA76167 Repair 1663M24P01 MAA17359 INSPECTED

3 Fan Blade 1590M21P01 MAAB3947 Repair 1663M24P01 MAA18489 INSPECTED

4 Fan Blade 1590M21P01 MAE18652-2 Repair 1663M24P01 MAA16666 INSPECTED

5 Fan Blade 1590M21P01 MAAB3953 Repair 1663M24P01 MAA18220 INSPECTED

6 Fan Blade 1590M21P01 MAA82012 Repair 1663M24P01 SNE17196 INSPECTED

7 Fan Blade 1590M21P01 MAAA9906 Repair 1663M24P01 MAA51290 INSPECTED

8 Fan Blade 1663M24P01 MAA64801 Scrap 1663M24P01 MAA38584 INSPECTED

9 Fan Blade 1663M24P01 MAA53086 Scrap 1663M24P01 MAA16625 INSPECTED

10 Fan Blade 1590M21P01 MAA94729 Scrap 1663M24P01 MAA17284 INSPECTED

11 Fan Blade 1590M21P01 MAAB4285 Scrap 1663M24P01 MAA34928 INSPECTED

12 Fan Blade 1590M21P01 MAAB4530 Repair 1663M24P01 MAA14537 INSPECTED

13 Fan Blade 1590M21P01 MAAA9913 Repair 1663M24P01 MAA25832 INSPECTED

14 Fan Blade 1590M21P01 MAAB4265 Repair 1663M24P01 MAA18205 INSPECTED

15 Fan Blade 1663M24P02 MAA71919 Repair 1663M24P01 MAA42642 INSPECTED

Page 56: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 7 of 55

No Disassembly Assembly

Description P/N S/N Remark P/N S/N Remark

16 Fan Blade 1663M24P01 MAA16944 Repair 1663M24P01 MAA18205 INSPECTED

17 Fan Blade 1590M21P01 KGAL1168 Repair 1663M24P01 MAA32368 INSPECTED

18 Fan Blade 1663M24P01 MAA57707 Repair 1663M24P01 MAA19607 INSPECTED

19 Fan Blade 1590M21P01 SNU69538 Repair 1663M24P01 MAA38571 INSPECTED

20 Fan Blade 1590M21P01 MAAB4532 Repair 1663M24P01 MAA33034 INSPECTED

21 Fan Blade 1663M24P02 MAA45795 Repair 1663M24P01 MAA25691 INSPECTED

22 Fan Blade 1663M24P02 MAA62190 Repair 1663M24P01 MAA28010 INSPECTED

23 Fan Blade 1663M24P01 MAA57804 Repair 1663M24P01 MAA26776 INSPECTED

24 Fan Blade 1590M21P01 MAAB3949 Repair 1663M24P01 MAA19810 INSPECTED

25 Fan Blade 1663M24P02 MAA75358 Repair 1663M24P01 MAA13795 INSPECTED

26 Fan Blade 1663M24P01 MAA64805 Repair 1663M24P01 MAA49658 INSPECTED

27 Fan Blade 1663M24P01 MAA61548 Repair 1663M24P01 MAA16862 INSPECTED

28 Fan Blade 1590M21P01 MAE18911-2 Repair 1663M24P01 MAA26619 INSPECTED

29 Fan Blade 1590M21P01 MAAB3952 Repair 1663M24P01 MAA26491 INSPECTED

30 Fan Blade 1590M21P01 MAAB4544 Repair 1663M24P01 SNE02714 INSPECTED

31 Fan Blade 1590M21P01 MAAB4145 Repair 1663M24P01 MAA14372 INSPECTED

32 Fan Blade 1590M21P01 MAAB4006 Repair 1663M24P01 MAA27259 INSPECTED

33 Fan Blade 1590M21P01 MAE28881-W Repair 1663M24P01 MAA17269 INSPECTED

34 Fan Blade 1590M21P01 KGAL2206 Repair 1663M24P01 MAA15157 INSPECTED

35 Fan Blade 1663M24P01 MAA56355 Repair 1663M24P01 MAA27587 INSPECTED

36 Fan Blade 1590M21P01 MAAB4540 Repair 1663M24P01 MAA31965 INSPECTED

37 Fan Blade 1590M21P01 MAA97245 Repair 1663M24P01 MAA28908 INSPECTED

Page 57: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 8 of 55

No Disassembly Assembly

Description P/N S/N Remark P/N S/N Remark

38 Fan Blade 1663M24P02 SNE19498 Repair 1663M24P01 MAA14288 REPAIRED

39 HPT1 NGV 2080M29G03 AMDP0112 Repair 2080M29G01 AMDC4545 Ex Overhaul

40 HPT1 NGV 2002M64G02 CN010206 Repair 2080M29G01 MDK0FR8G

Ex Overhaul

41 HPT1 NGV 2080M29G03 AMDF2533 Repair 2080M29G01 AMDK6071

Ex Overhaul

42 HPT1 NGV 2002M64G02 CN09927 Repair 2080M29G01 AMDF7403

Ex Overhaul

43 HPT1 NGV 2080M29G03 AMDL6328 Repair 2080M29G01 AMDN702

Ex Overhaul

44 HPT1 NGV 2002M64G02 CN10461 Repair 2080M29G01 D01621

Ex Overhaul

45 HPT1 NGV 2002M64G02 CN05772 Repair 2080M29G01 AMDN5598

Ex Overhaul

46 HPT1 NGV 2080M29G03 AMDN4814 Repair 2080M29G01 HCM00369

Ex Overhaul

47 HPT1 NGV 2080M29G03 AMD4M899 Repair 2080M29G01 AMDK8641

Ex Overhaul

48 HPT1 NGV 2002M64G02 CN09901 Repair 2080M29G01 AMDE8087

Ex Overhaul

49 HPT1 NGV 2080M29G03 AMDD9273 Repair 2080M29G01 AMDAT927

Ex Overhaul

50 HPT1 NGV 2080M29G03 AMD19183 Repair 2080M29G01 AMDK5743

Ex Overhaul

51 HPT1 NGV 2080M29G03 AMDL0077 Repair 2080M29G01 AMDB3022

Ex Overhaul

52 HPT1 NGV 2080M29G03 AMDG3159 Repair 2080M29G01 AMD4M169

Ex Overhaul

53 HPT1 NGV 2002M64G02 CN09896 Repair 2080M29G01 AMDF4353

Ex Overhaul

54 HPT1 NGV 2080M29G03 AMDC5819 Repair 2080M29G01 AMDK3810

Ex Overhaul

55 HPT1 NGV 2002M64G02 CN10204 Repair 2080M29G01 ADAF163

Ex Overhaul

56 HPT1 NGV 2080M29G03 AMD6M516 Repair 2080M29G01 MDK0D6JJ

Ex Overhaul

57 HPT1 NGV 2002M64G02 CN45GYJ Repair 2080M29G01 AMD0N245

Ex Overhaul

58 HPT1 NGV 2002M64G02 CN34638 Repair 2080M29G01 AMDH5909

Ex Overhaul

59 HPT1 NGV 2080M29G03 AMDG3195 Repair 2080M29G01 AMDD1360

Ex Overhaul

Page 58: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 9 of 55

No Disassembly Assembly

Description P/N S/N Remark P/N S/N Remark

60 HPT1 NGV 2002M64G02 CN45BAD Repair 2080M29G01 AMDAC248 Ex Overhaul

61 HPT1 NGV 2080M29G03 CN462XC Repair 2080M29G01 MDK0AAPJ Ex Overhaul

62 HPTR Blade 1475M35P01 STB99 Scrap 1475M35P02 0FD5 Ex Overhaul

63 HPTR Blade 1475M35P01 46M57 Scrap 1475M35P02 1296 Ex Overhaul

64 HPTR Blade 1475M35P01 877M4 Scrap 1475M35P02 1767 Ex Overhaul

65 HPTR Blade 1475M35P01 884M4 Scrap 1475M35P02 160D Ex Overhaul 66 67

HPTR Blade 1668M23P01 6W977 Scrap 1475M35P02 15C7

Ex Overhaul

68 HPTR Blade 1475M35P01 SNN24 Scrap 1475M35P02 16A4 Ex Overhaul

69 HPTR Blade 1475M35P01 FHN26 Scrap 1475M35P02 1784 Ex Overhaul

70 HPTR Blade 1475M35P01 73N75 Scrap 1475M35P02 1A29 Ex Overhaul

71 HPTR Blade 1475M35P01 680M6 Scrap 1475M35P02 1222 Ex Overhaul

72 HPTR Blade 1475M35P01 463N1 Scrap 1475M35P02 18C4 Ex Overhaul

73 HPTR Blade 1475M35P01 74N72 Scrap 1475M35P02 2FDA Ex Overhaul

74 HPTR Blade 1475M35P01 440M6 Scrap 1475M35P02 1A40 Ex Overhaul

75 HPTR Blade 1475M35P01 0974N Scrap 1475M35P02 2BB0 Ex Overhaul

76 HPTR Blade 1475M35P01 946M4 Scrap 1475M35P02 1A62 Ex Overhaul

77 HPTR Blade 1475M35P01 46CL2 Scrap 1475M35P02 195E Ex Overhaul

78 HPTR Blade 1475M35P01 949M5 Scrap 1475M35P02 165D Ex Overhaul

79 HPTR Blade 1475M35P01 981M1 Scrap 1475M35P02 1A3A Ex Overhaul

80 HPTR Blade 1475M35P01 024R2 Scrap 1475M35P02 1AD3 Ex Overhaul

81 HPTR Blade 1668M23P01 94N97 Scrap 1475M35P02 13C3 Ex Overhaul

82 HPTR Blade 1668M23P01 AD670 Scrap 1475M35P02 1A05 Ex Overhaul

Page 59: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 10 of 55

No Disassembly Assembly

Description P/N S/N Remark P/N S/N Remark

83 HPTR Blade 1668M23P01 OM981 Scrap 1475M35P02 15B7 Ex Overhaul

84 HPTR Blade 1475M35P01 SNU62 Scrap 1475M35P02 17D5 Ex Overhaul

85 HPTR Blade 1475M35P01 FJB92 Scrap 1475M35P02 1891 Ex Overhaul

86 HPTR Blade 1668M23P01 7065J Scrap 1475M35P02 1916 Ex Overhaul

87 HPTR Blade 1668M23P01 3576K Scrap 1475M35P02 193E Ex Overhaul

88 HPTR Blade 1475M35P01 46CB7 Scrap 1475M35P02 1AB7 Ex Overhaul

89 HPTR Blade 1475M35P01 1687N Scrap 1475M35P02 1ABA Ex Overhaul

90 HPTR Blade 1475M35P01 701M2 Scrap 1475M35P02 1ABC Ex Overhaul

91 HPTR Blade 1668M23P01 OM857 Scrap 1475M35P02 1AA5 Ex Overhaul

92 HPTR Blade 1475M35P01 36N82 Scrap 1475M35P02 17B8 Ex Overhaul

93 HPTR Blade 1668M23P01 4333K Scrap 1475M35P02 1985 Ex Overhaul

94 HPTR Blade 1475M35P01 GRL26 Scrap 1475M35P02 CE50 Ex Overhaul

95 HPTR Blade 1668M23P01 97137 Scrap 1475M35P02 1A59 Ex Overhaul

96 HPTR Blade 1475M35P01 SNV30 Scrap 1475M35P02 1786 Ex Overhaul

97 HPTR Blade 1475M35P01 49N75 Scrap 1475M35P02 1845 Ex Overhaul

98 HPTR Blade 1475M35P01 SNM44 Scrap 1475M35P02 190E Ex Overhaul

99 HPTR Blade 1475M35P01 803M0 Scrap 1475M35P02 1353 Ex Overhaul

100 HPTR Blade 1475M35P01 SNJ88 Scrap 1475M35P02 15CD Ex Overhaul

101 HPTR Blade 1475M35P01 761M6 Scrap 1475M35P02 18B1 Ex Overhaul

102 HPTR Blade 1475M35P01 013R2 Scrap 1475M35P02 16A3 Ex Overhaul

103 HPTR Blade 1475M35P01 681M8 Scrap 1475M35P02 198E Ex Overhaul

104 HPTR Blade 1475M35P01 8L281 Scrap 1475M35P02 1827 Ex Overhaul

Page 60: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 11 of 55

No Disassembly Assembly

Description P/N S/N Remark P/N S/N Remark

105 HPTR Blade 1668M23P01 0949R Scrap 1475M35P02 1636 Ex Overhaul

106 HPTR Blade 1668M23P01 96N30 Scrap 1475M35P02 1AC7 Ex Overhaul

107 HPTR Blade 1668M23P01 0AM66 Scrap 1475M35P02 2D3B Ex Overhaul

108 HPTR Blade 1475M35P01 228N4 Scrap 1475M35P02 1582 Ex Overhaul

109 HPTR Blade 1668M23P01 5148K Scrap 1475M35P02 1904 Ex Overhaul

110 HPTR Blade 1475M35P01 SNK81 Scrap 1475M35P02 186C Ex Overhaul

111 HPTR Blade 1475M35P01 SNY71 Scrap 1475M35P02 1A70 Ex Overhaul

112 HPTR Blade 1668M23P01 80N72 Scrap 1475M35P02 1918 Ex Overhaul

113 HPTR Blade 1475M35P01 0866N Scrap 1475M35P02 14D0 Ex Overhaul

114 HPTR Blade 1668M23P01 8372H Scrap 1475M35P02 19A3 Ex Overhaul

115 HPTR Blade 1668M23P01 2467K Scrap 1475M35P02 1933 Ex Overhaul

116 HPTR Blade 1475M35P01 SNM36 Scrap 1475M35P02 1A04 Ex Overhaul

117 HPTR Blade 1475M35P01 SNL14 Scrap 1475M35P02 0FD7 Ex Overhaul

118 HPTR Blade 1475M35P01 93YN1 Scrap 1475M35P02 17BB Ex Overhaul

119 HPTR Blade 1475M35P01 SNN07 Scrap 1475M35P02 15C2 Ex Overhaul

120 HPTR Blade 1475M35P01 SLA40 Scrap 1475M35P02 1AC2 Ex Overhaul

121 HPTR Blade 1475M35P01 45JU7 Scrap 1475M35P02 10D6 Ex Overhaul

122 HPTR Blade 1668M23P01 J5367 Scrap 1475M35P02 0FF0 Ex Overhaul

123 HPTR Blade 1475M35P01 868M1 Scrap 1475M35P02 03C2 Ex Overhaul

124 HPTR Blade 1475M35P01 FGM34 Scrap 1475M35P02 1AD2 Ex Overhaul

125 HPTR Blade 1668M23P01 5858H Scrap 1475M35P02 2F6D Ex Overhaul

126 HPTR Blade 1668M23P01 7180K Scrap 1475M35P02 191F Ex Overhaul

Page 61: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 12 of 55

No Disassembly Assembly

Description P/N S/N Remark P/N S/N Remark

127 HPTR Blade 1475M35P01 028R6 Scrap 1475M35P02 1722 Ex Overhaul

128 HPTR Blade 1668M23P01 38N65 Scrap 1475M35P02 1762 Ex Overhaul

129 HPTR Blade 1475M35P01 800M9 Scrap 1475M35P02 15CB Ex Overhaul

130 HPTR Blade 1475M35P01 3774M Scrap 1475M35P02 16C4 Ex Overhaul

131 HPTR Blade 1475M35P01 SNB97 Scrap 1475M35P02 162B Ex Overhaul

132 HPTR Blade 1475M35P01 912N9 Scrap 1475M35P02 1AC6 Ex Overhaul

133 HPTR Blade 1668M23P01 96N82 Scrap 1475M35P02 1240 Ex Overhaul

134 HPT Shroud

135 LPT1 NGV 305-350-059-0 RN75520 Repair 305-350-058-0 RN00080 Ex Overhaul

136 LPT1 NGV 305-350-059-0 RN21302 Repair 305-350-058-0 J32715D Ex Overhaul

137 LPT1 NGV 305-350-059-0 RN10661 Repair 305-350-058-0 J29019C Ex Overhaul

138 LPT1 NGV 305-350-059-0 DA894639-0 Repair 305-350-058-0 J34127B Ex Overhaul

139 LPT1 NGV 305-350-059-0 RN13862 Repair 305-350-058-0 J9E3787

Ex Overhaul

140 LPT1 NGV 305-350-059-0 RN20208 Repair 305-350-058-0 RN02719 Ex Overhaul

141 LPT1 NGV 305-350-059-0 RN10862 Repair 305-350-058-0 J13296D Ex Overhaul

142 LPT1 NGV 305-350-059-0 RN20281 Repair 305-350-058-0 RN03077 Ex Overhaul

143 LPT1 NGV 305-350-059-0 RN35838 Repair 305-350-058-0 J12907A Ex Overhaul

144 LPT1 NGV 305-350-059-0 RN09590 Repair 305-350-058-0 J9E4166 Ex Overhaul

145 LPT1 NGV 305-350-059-0 J250160 Repair 305-350-058-0 J27671C Ex Overhaul

146 LPT1 NGV 305-350-059-0 J510610 Repair 305-350-058-0 J25932D Ex Overhaul

147 LPT1 NGV 305-350-059-0 RN10252 Repair 305-350-058-0 J9E1017 Ex Overhaul

Page 62: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 8 of 55

No Disassembly Assembly

Description P/N S/N Remark P/N S/N Remark

38 Fan Blade 1663M24P02 SNE19498 Repair 1663M24P01 MAA14288 REPAIRED

39 HPT1 NGV 2080M29G03 AMDP0112 Repair 2080M29G01 AMDC4545 Ex Overhaul

40 HPT1 NGV 2002M64G02 CN010206 Repair 2080M29G01 MDK0FR8G Ex Overhaul

41 HPT1 NGV 2080M29G03 AMDF2533 Repair 2080M29G01 AMDK6071 Ex Overhaul

42 HPT1 NGV 2002M64G02 CN09927 Repair 2080M29G01 AMDF7403 Ex Overhaul

43 HPT1 NGV 2080M29G03 AMDL6328 Repair 2080M29G01 AMDN702 Ex Overhaul

44 HPT1 NGV 2002M64G02 CN10461 Repair 2080M29G01 D01621 Ex Overhaul

45 HPT1 NGV 2002M64G02 CN05772 Repair 2080M29G01 AMDN5598 Ex Overhaul

46 HPT1 NGV 2080M29G03 AMDN4814 Repair 2080M29G01 HCM00369 Ex Overhaul

47 HPT1 NGV 2080M29G03 AMD4M899 Repair 2080M29G01 AMDK8641 Ex Overhaul

48 HPT1 NGV 2002M64G02 CN09901 Repair 2080M29G01 AMDE8087 Ex Overhaul

49 HPT1 NGV 2080M29G03 AMDD9273 Repair 2080M29G01 AMDAT927 Ex Overhaul

50 HPT1 NGV 2080M29G03 AMD19183 Repair 2080M29G01 AMDK5743 Ex Overhaul

51 HPT1 NGV 2080M29G03 AMDL0077 Repair 2080M29G01 AMDB3022 Ex Overhaul

52 HPT1 NGV 2080M29G03 AMDG3159 Repair 2080M29G01 AMD4M169 Ex Overhaul

53 HPT1 NGV 2002M64G02 CN09896 Repair 2080M29G01 AMDF4353 Ex Overhaul

54 HPT1 NGV 2080M29G03 AMDC5819 Repair 2080M29G01 AMDK3810 Ex Overhaul

55 HPT1 NGV 2002M64G02 CN10204 Repair 2080M29G01 ADAF163 Ex Overhaul

56 HPT1 NGV 2080M29G03 AMD6M516 Repair 2080M29G01 MDK0D6JJ Ex Overhaul

57 HPT1 NGV 2002M64G02 CN45GYJ Repair 2080M29G01 AMD0N245 Ex Overhaul

58 HPT1 NGV 2002M64G02 CN34638 Repair 2080M29G01 AMDH5909 Ex Overhaul

59 HPT1 NGV 2080M29G03 AMDG3195 Repair 2080M29G01 AMDD1360 Ex Overhaul

Page 63: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 9 of 55

No Disassembly Assembly

Description P/N S/N Remark P/N S/N Remark

60 HPT1 NGV 2002M64G02 CN45BAD Repair 2080M29G01 AMDAC248 Ex Overhaul

61 HPT1 NGV 2080M29G03 CN462XC Repair 2080M29G01 MDK0AAPJ Ex Overhaul

62 HPTR Blade 1475M35P01 STB99 Scrap 1475M35P02 0FD5 Ex Overhaul

63 HPTR Blade 1475M35P01 46M57 Scrap 1475M35P02 1296 Ex Overhaul

64 HPTR Blade 1475M35P01 877M4 Scrap 1475M35P02 1767 Ex Overhaul

65 HPTR Blade 1475M35P01 884M4 Scrap 1475M35P02 160D Ex Overhaul 66 67

HPTR Blade 1668M23P01 6W977 Scrap 1475M35P02 15C7

Ex Overhaul

68 HPTR Blade 1475M35P01 SNN24 Scrap 1475M35P02 16A4 Ex Overhaul

69 HPTR Blade 1475M35P01 FHN26 Scrap 1475M35P02 1784 Ex Overhaul

70 HPTR Blade 1475M35P01 73N75 Scrap 1475M35P02 1A29 Ex Overhaul

71 HPTR Blade 1475M35P01 680M6 Scrap 1475M35P02 1222 Ex Overhaul

72 HPTR Blade 1475M35P01 463N1 Scrap 1475M35P02 18C4 Ex Overhaul

73 HPTR Blade 1475M35P01 74N72 Scrap 1475M35P02 2FDA Ex Overhaul

74 HPTR Blade 1475M35P01 440M6 Scrap 1475M35P02 1A40 Ex Overhaul

75 HPTR Blade 1475M35P01 0974N Scrap 1475M35P02 2BB0 Ex Overhaul

76 HPTR Blade 1475M35P01 946M4 Scrap 1475M35P02 1A62 Ex Overhaul

77 HPTR Blade 1475M35P01 46CL2 Scrap 1475M35P02 195E Ex Overhaul

78 HPTR Blade 1475M35P01 949M5 Scrap 1475M35P02 165D Ex Overhaul

79 HPTR Blade 1475M35P01 981M1 Scrap 1475M35P02 1A3A Ex Overhaul

80 HPTR Blade 1475M35P01 024R2 Scrap 1475M35P02 1AD3 Ex Overhaul

81 HPTR Blade 1668M23P01 94N97 Scrap 1475M35P02 13C3 Ex Overhaul

82 HPTR Blade 1668M23P01 AD670 Scrap 1475M35P02 1A05 Ex Overhaul

Page 64: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 12 of 55

No Disassembly Assembly

Description P/N S/N Remark P/N S/N Remark

127 HPTR Blade 1475M35P01 028R6 Scrap 1475M35P02 1722 Ex Overhaul

128 HPTR Blade 1668M23P01 38N65 Scrap 1475M35P02 1762 Ex Overhaul

129 HPTR Blade 1475M35P01 800M9 Scrap 1475M35P02 15CB Ex Overhaul

130 HPTR Blade 1475M35P01 3774M Scrap 1475M35P02 16C4 Ex Overhaul

131 HPTR Blade 1475M35P01 SNB97 Scrap 1475M35P02 162B Ex Overhaul

132 HPTR Blade 1475M35P01 912N9 Scrap 1475M35P02 1AC6 Ex Overhaul

133 HPTR Blade 1668M23P01 96N82 Scrap 1475M35P02 1240 Ex Overhaul

134 HPT Shroud

135 LPT1 NGV 305-350-059-0 RN75520 Repair 305-350-058-0 RN00080 Ex Overhaul

136 LPT1 NGV 305-350-059-0 RN21302 Repair 305-350-058-0 J32715D Ex Overhaul

137 LPT1 NGV 305-350-059-0 RN10661 Repair 305-350-058-0 J29019C Ex Overhaul

138 LPT1 NGV 305-350-059-0 DA894639-0 Repair 305-350-058-0 J34127B Ex Overhaul

139 LPT1 NGV 305-350-059-0 RN13862 Repair 305-350-058-0 J9E3787

Ex Overhaul

140 LPT1 NGV 305-350-059-0 RN20208 Repair 305-350-058-0 RN02719 Ex Overhaul

141 LPT1 NGV 305-350-059-0 RN10862 Repair 305-350-058-0 J13296D Ex Overhaul

142 LPT1 NGV 305-350-059-0 RN20281 Repair 305-350-058-0 RN03077 Ex Overhaul

143 LPT1 NGV 305-350-059-0 RN35838 Repair 305-350-058-0 J12907A Ex Overhaul

144 LPT1 NGV 305-350-059-0 RN09590 Repair 305-350-058-0 J9E4166 Ex Overhaul

145 LPT1 NGV 305-350-059-0 J250160 Repair 305-350-058-0 J27671C Ex Overhaul

146 LPT1 NGV 305-350-059-0 J510610 Repair 305-350-058-0 J25932D Ex Overhaul

147 LPT1 NGV 305-350-059-0 RN10252 Repair 305-350-058-0 J9E1017 Ex Overhaul

Page 65: YTE LH 722283...CFM56-3, 3B, 3C TO PREVENT AGB STARTER GEARSHAFT FAILURE,WHICH COULD RESULT IN IFSD AND FORCED LANDING. N/A Replace suspected gearshaft within 350 hrs TIS after the

Maintenance Report ESN: 722283 Page 13 of 55

No Disassembly Assembly

Description P/N S/N Remark P/N S/N Remark

148 LPT1 NGV 305-350-059-0 RN46902 Repair 305-350-058-0 J23473B Ex Overhaul

149 LPT1 NGV 305-350-059-0 RN46884 Repair 305-350-058-0 J32981D Ex Overhaul

150 LPT1 NGV 305-350-059-0 J25263A Repair 305-350-058-0 J9E4546 Ex Overhaul

151 LPT1 NGV 305-350-059-0 J50257B Repair 305-350-058-0 J9F7478 Ex Overhaul

152 LPT1 NGV 305-350-059-0 RN13181 Repair 305-350-058-0 J33100B Ex Overhaul

153 LPT1 NGV 305-350-059-0 RN10885 Repair 305-350-058-0 J9F0632 Ex Overhaul

154 LPT1 NGV 305-350-059-0 J501558 Repair 305-350-058-0 J27213C Ex Overhaul

155 LPT1 NGV 305-350-059-0 RN20851 Repair 305-350-058-0 J9E9167 Ex Overhaul

156 LPT1 NGV 305-350-059-0 J501668 Repair 305-350-058-0 RN03152 Ex Overhaul

157 LPT1 NGV 305-350-059-0 J51286D Repair 305-350-058-0 J33504A Ex Overhaul

158 LPT1 NGV 305-350-059-0 RN156129 Repair 305-350-057-0 J9F0191 EX esn 720697 159 LPT1 NGV 305-350-059-0 RN10818 Repair 305-350-057-0

J32716B EX esn 720697

160 LPT1 NGV 305-350-059-0 RN09624 Repair 305-350-057-0 J02977B

EX esn 720697

161 LPT1 NGV 305-350-159-0 RN134779 Repair 305-350-057-0 J00924B

EX esn 720697

162 LPT1 NGV 305-350-159-0 RN13761 Repair 305-350-057-0 J11280

EX esn 720697

163 LPT Major Module - 54X22283 Due LLP - 54X20283 Ex esn 720283