Copy · PASSPORT20 SB 72-00-0116-00A-930A-D Aug 13 2021 · 11 pages

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PASSPORT20 Service Bulletins (SBs) 72-00-0116-00A-930A-D - 002 - ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service Date Printed:

2022/01/05 GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical data is considered ITAR and/or EAR controlled;

transfer of this data to a Non-US Person, without USG authorization, is strictly prohibited.

Page 1 of 11 ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service Service bulletin DMC: PASSPORT20-A-72-00-0116-00A-930A-D Language: sx/US Issue No: 002 Issue Date: 13 Aug 2021 Title: ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service - Service bulletin DM Status Security classification: Class01 Responsible Company: GE Passport LLC (80NQ3) Originator: GE Passport LLC (80NQ3) Applicability: EngineRating All Reason(s) for update:

* Update technical content.[Technical] GE Designated: -CONFIDENTIAL- The information contained in this document is GE proprietary information and is disclosed in confidence. It is the property of GE and shall not be used, disclosed to others or reproduced without the express written consent of GE, including, but without limitation, it is not to be used in the creation, manufacture, development, or derivation of any repairs, modifications, spare parts, designs, or configuration changes or to obtain FAA or any other government or regulatory approval to do so. If consent is given for reproduction in whole or in part, this notice and the notice set forth on each page of this document shall appear in any such reproduction in whole or part.

This technical data is considered subject to the Export Administration Regulations (EAR) pursuant to 15 CFR Parts 730-774. Transfer of this data by any means to a Non-U.S. Person, whether in the United States or abroad, without the proper U.S. Government authorization (e.g., License, exemption, NLR, etc.), is strictly prohibited.

Copyright (2021) General Electric Company, U.S.A.

PASSPORT20 Service Bulletins (SBs) 72-00-0116-00A-930A-D - 002 - ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service Date Printed:

2022/01/05 GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical data is considered ITAR and/or EAR controlled;

transfer of this data to a Non-US Person, without USG authorization, is strictly prohibited.

Page 2 of 11 Table of contents:

1. References

2. Revision Information A. Revision reason B. Revision history C. Revision sequence

3. Summary A. Summary

4. Planning Information A. Applicability B. Concurrent requirements C. Reason D. Description E. Compliance F. Approval G. Manpower H. Weight and balance I. Electrical load data J. Software accomplishment summary K. Referenced documentation L. Documentation affected M. Industry support information N. Interchangeability

5. Material Information

6. Accomplishment Instructions

7. Additional Information

PASSPORT20 Service Bulletins (SBs) 72-00-0116-00A-930A-D - 002 - ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service Date Printed:

2022/01/05 GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical data is considered ITAR and/or EAR controlled;

transfer of this data to a Non-US Person, without USG authorization, is strictly prohibited.

Page 3 of 11 List of figures:

1 HPTR stage 1 disk

PASSPORT20 Service Bulletins (SBs) 72-00-0116-00A-930A-D - 002 - ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service Date Printed:

2022/01/05 GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical data is considered ITAR and/or EAR controlled;

transfer of this data to a Non-US Person, without USG authorization, is strictly prohibited.

Page 4 of 11 List of tables:

1 HPTR stage 1 disk (158A0, 2471M11P02) serial numbers

1. References Table: References Data Module/Technical Publication Title PASSPORT20-A-05-11-03-00A-0B1A-D HPT Rotor - Life Limits PASSPORT20-A-72-53-00-19A-530A-C High pressure turbine rotor assembly (Stage 1 disk assembly toforward shaft/FOS, stage 2 disk) - Disassemble procedure Management Information Manufacturer recommendation: Mandatory Task Type Administrative Original issue date 2020/08/07

2. Revision Information A. Revision reason Issue Number Revision Reason 001 Baseline 002 To update the Service Bulletin paragraph 4. Planning Information.

B. Revision history Issue Number Issue Date 001 2020/08/07 002 2021/08/13 C. Revision sequence Issue 002.

3. Summary A. Summary This service bulletin removes from service a population of stage 1 disks (158A0) due to potentialhigh pressure turbine rotor (HPTR) dimensional non-conformances from new-make manufacturing.

4. Planning Information A. Applicability This service bulletin is applicable to stage 1 disks, P/N 2471M11P02, with the serial numbers contained in HPTR Table 1 - HPTR stage 1 .disk (158A0, 2471M11P02) serial numbers These serial numbers are the best available data.

PASSPORT20 Service Bulletins (SBs) 72-00-0116-00A-930A-D - 002 - ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service Date Printed:

2022/01/05 GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical data is considered ITAR and/or EAR controlled;

transfer of this data to a Non-US Person, without USG authorization, is strictly prohibited.

Page 5 of 11 Table 1: HPTR stage 1 disk (158A0, 2471M11P02) serial numbers Serial number Serial number Serial number FIA12J6W FIA19FCE FIA1L1KH FIA12J6Y FIA19FCH FIA1L1KK FIA13KRA FIA19FCJ FIA1LFFE FIA13KRE FIA19FCK FIA1LFFF FIA13KRF FIA19FCL FIA1LFFH FIA13KRH FIA19FCP FIA1LFFJ FIA14GJJ FIA19J85 FIA1LFFK FIA14GK0 FIA19J87 FIA1LFFL FIA14GK3 FIA19J88 FIA1N53P FIA14GK5 FIA19J89 FIA1N53R FIA14GK8 FIA19J94 FIA1N53W FIA14GK9 FIA19J9A FIA1N54C FIA14GLE FIA19J9C FIA1N54E FIA14GLF FIA19J9E FIA1NFJH FIA14GLJ FIA19J9F FIA1NFJJ FIA14WC2 FIA19J9H FIA1NFJK FIA14WC6 FIA19J9J FIA1P57F FIA14WC9 FIA19J9L FIA1P57H FIA176R2 FIA19YK4 FIA1P57J FIA176R3 FIA19YK5 FIA1P57K FIA176R4 FIA19YK6 FIA1P57L FIA176R5 FIA19YK8 FIA1P57P FIA176R6 FIA19YK9 FIA1P82R FIA17LY0 FIA1KANJ FIA1P82T FIA17LY2 FIA1KANK FIA1P82W FIA17LY3 FIA1KANL FIA1P82Y FIA17LYT FIA1KANP FIA1P83A FIA17LYW FIA1KANR FIA1P83C FIA184C1 FIA1KANT FIA1P93T FIA184C2 FIA1KCFE FIA1P93W FIA184C4 FIA1KCFF FIA1P93Y FIA184C5 FIA1KCFH FIA1P94A FIA18ET0 FIA1KCFJ FIA1P94C FIA18ET1 FIA1KCFK FIA1P94E FIA18ET2 FIA1KCFL FIA1PA08 FIA18ETW FIA1KCFP FIA1PA09 FIA18ETY FIA1KK00 FIA1PA1A FIA18P40 FIA1KK01 FIA1PA1C

PASSPORT20 Service Bulletins (SBs) 72-00-0116-00A-930A-D - 002 - ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service Date Printed:

2022/01/05 GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical data is considered ITAR and/or EAR controlled;

transfer of this data to a Non-US Person, without USG authorization, is strictly prohibited.

Page 6 of 11

1.

2.

3.

4.

5.

FIA18P41 FIA1KK0R FIA1PA1E FIA18P4R FIA1KK0W FIA1PA1F FIA18P4T FIA1KK0Y FIA1PEL6 FIA18P4W FIA1KK10 FIA1PEL7 FIA18P4Y FIA1KN38 FIA1PEL8 FIA18W29 FIA1KN39 FIA1PELK FIA18W3A FIA1KN4A FIA1PELL FIA18W3C FIA1KN4C FIA1PELP FIA18W3E FIA1KN4F FIA1PP84 FIA18W3F FIA1L1KA FIA1PP85 FIA18W3H FIA1L1KC FIA1PP87 FIA18W3J FIA1L1KE FIA1PP88 FIA18W3K FIA1L1KF FIA18W3L B. Concurrent requirements None.

C. Reason Objective:

To remove from service a suspect population of parts.

Condition:

The forward and aft hooks of stage 1 disks identified by the serial numbers are potentially non-conforming.HPTR Cause:

Machining and inspection on the serial numbered stage 1 disks was found to be inconsistent with the engineering drawing.HPTR Improvement:

The stage 1 disks specified by serial number in this service bulletin are to be removed from service no later than the cycle limitHPTR defined.

Substantiation:

Analysis and comparative analysis.

This service bulletin complements the changes made to the HPT Rotor - Life Limits (DMC-PASSPORT20-A-05-11-03-00A-0B1A-D) . The removal from service for the population herein within the required cycles of 05-11-03 maintains airworthiness.

D. Description The purpose of this service bulletin is to require removal from service the stage 1 disk identified by serial numbers.HPTR E. Compliance Category 1 GE recommends that you do this service bulletin before 3800 cycles.

Impact A This recommendation is to address a condition that may affect flight safety.

Note: This service bulletin can be done in the engine shop.

F. Approval The data contained in this service bulletin has been reviewed by the FAA or authorized entity representing the FAA and repair(s) and modification(s) herein comply with the applicable aviation regulations and are APPROVED for installation in the model(s) listed in this service bulletin.

G. Manpower You will need approximately one man-hour after piece-part exposure to comply with this service bulletin.

H. Weight and balance Weight and balance are not changed I. Electrical load data Not applicable.

PASSPORT20 Service Bulletins (SBs) 72-00-0116-00A-930A-D - 002 - ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service Date Printed:

2022/01/05 GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical data is considered ITAR and/or EAR controlled;

transfer of this data to a Non-US Person, without USG authorization, is strictly prohibited.

Page 7 of 11 J. Software accomplishment summary Not applicable.

K. Referenced documentation Note: The reference documents listed below are for the engine manufacturer's internal use only:

BPP/EPEX No. 20-72-53-92451 and BPP/PCM No. 8000345 QEM No. 37529-20-107 MTDC P20-2020-MT-040 and P20-2021-MT-042 L. Documentation affected GEK 112062, Passport 20 Line Maintenance Manual (LMM) M. Industry support information GE is pleased to offer support for incorporation of this service bulletin.

* Contact your GE Aviation regional account leader for details of the support.

N. Interchangeability Not applicable

5. Material Information List of material sets None List of support equipment None List of supplies None List of spares None List of removed spares None

6. Accomplishment Instructions A. Replace the suspect HPTR stage 1 disk. Refer to Figure 1

PASSPORT20 Service Bulletins (SBs) 72-00-0116-00A-930A-D - 002 - ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service Date Printed:

2022/01/05 GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical data is considered ITAR and/or EAR controlled;

transfer of this data to a Non-US Person, without USG authorization, is strictly prohibited.

Page 8 of 11 Figure 1: HPTR stage 1 disk

PASSPORT20 Service Bulletins (SBs) 72-00-0116-00A-930A-D - 002 - ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service Date Printed:

2022/01/05 GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical data is considered ITAR and/or EAR controlled;

transfer of this data to a Non-US Person, without USG authorization, is strictly prohibited.

Page 9 of 11 .

(1) Disassemble the HPTR to piece part level. Refer to High pressure turbine rotor assembly (Stage 1 disk assembly to forward shaft/FOS, .stage 2 disk) - Disassemble procedure (DMC-PASSPORT20-A-72-53-00-19A-530A-C)

(2) Remove from service and contact Fleet Support to return the stage 1 disk (158A0) to GE. Refer to this service bulletin and giveHPTR the stage 1 disk serial number.HPTR

7. Additional Information None Figure 1 - HPTR stage 1 disk

PASSPORT20 Service Bulletins (SBs) 72-00-0116-00A-930A-D - 002 - ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service Date Printed:

2022/01/05 GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical data is considered ITAR and/or EAR controlled;

transfer of this data to a Non-US Person, without USG authorization, is strictly prohibited.

Page 10 of 11 Figure 1 - HPTR stage 1 disk: HPTR stage 1 disk

PASSPORT20 Service Bulletins (SBs) 72-00-0116-00A-930A-D - 002 - ENGINE - High pressure turbine (72-53-02) - Stage 1 disk - Removal from service Date Printed:

2022/01/05 GE PROPRIETARY INFORMATION - Not to be used, disclosed to others or reproduced without the express written consent of GE. Technical data is considered ITAR and/or EAR controlled;

transfer of this data to a Non-US Person, without USG authorization, is strictly prohibited.

Page 11 of 11 GE Designated: - CONFIDENTIAL- Subject to the restrictions on the media PASSPORT20-A-72-00-0116-00A-930A-D Issue 002 - 2021-08-13