On this page
Copies · 2
Copies of this document that the FAA filed in AD dockets on regulations.gov, newest revision first. A newer revision may exist.
© Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2025-0611; AD 2026-02-07 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
© Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2025-0611; AD 2026-02-07 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Manufacturer
- Airbus
- Type
- Service Bulletin
- Number
- A350-32-P057
- Latest revision known
- A350-32-P057, Revision 01, dated December 12, 2024
- Copies
- 2 files of 1 revision
A newer revision may exist than any OpenAirDocs knows of: check with the manufacturer.
ADs that cite it · 1
Newest first, with the revision each names, as OpenAirDocs read it from the AD’s text: check it against the AD.
Text · 28
Revision 01, the newest copy. From the PDF’s text layer: layout, tables and figures are lost. The PDF is the document. © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2025-0611; AD 2026-02-07 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
Query with SQL
duckdb -csv -c "SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '9c075c04c4f48bb4e654d0bada8d4b2b779c797274b8573a59791e4b2095d487' ORDER BY p.page"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT p.page, p.text_source, p.text, f.rights_holder, f.license FROM 'https://openairdocs.org/data/latest/service_document_file_page.parquet' p JOIN 'https://openairdocs.org/data/latest/service_document_file.parquet' f USING (file_sha256) WHERE p.file_sha256 = '9c075c04c4f48bb4e654d0bada8d4b2b779c797274b8573a59791e4b2095d487' ORDER BY p.page
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
A350
SERVICE BULLETIN REV 00 Sep 30/24 A350-32-P057 Page 1
CONF ALL AIRBUS 2, ROND POINT EMILE DEWOITINE 31700 BLAGNAC FRANCE
The content of this document is the property of Airbus. All rights including copyrights are reserved.
It is supplied in confidence and commercial security on its contents must be maintained.
It must not be used for any purpose other than that for which it is supplied, nor may information contained in it be disclosed to unauthorized persons.
It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. Requests for reproduction of any data in this document and the media authorized for it must be addressed to Airbus.
MANDATORY MANDATORY MANDATORY ATA SYSTEM: 32 TITLE: LANDING GEAR - NOSE LANDING GEAR (NLG) - LOWER TORQUE
LINKS MISSING BRIGHT SHOT PEENING MODIFICATION No.:
None
A350
SERVICE BULLETIN
SUMMARY REV 00 Sep 30/24 A350-32-P057 Page 2 ATA SYSTEM: 32 TITLE: LANDING GEAR - NOSE LANDING GEAR (NLG) - LOWER TORQUE
LINKS MISSING BRIGHT SHOT PEENING
SUMMARY This summary is for information only and is not approved for modification of the aircraft.
A. MODIFICATIONS
MODIFICATION CLASSIFICATION MAJOR None MINOR None NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes.
B. REASON
(1) History During initial production of the Entry Into Service (EIS) standard NLG, some lower torque links (Part Number (PN) 5035-0401) were manufactured without bright shot peening. The omission of bright shot peening may reduce the life limitation of the component, depending on which aircraft weight variant and NLG standard the component is installed on.
(2) Objective/Action The objective of this Inspection Service Bulletin (ISB) is to give the required information for the operators to be able to determine for each affected lower torque link the new life limitation.
(3) Advantages The accomplishment of this ISB ensures that the right life for the affected torque link and therefore ensure to not exceed the correct life limitation.
(4) Operational/Maintenance Consequences None C. GENERAL EVALUATION
EVALUATION TABLE
COMPLIANCE MANDATORY COST SAVING NO
A/C OPERATION
AFFECTED
NO VENDOR SB NO
CANCELS INSPECTION SB NO ETOPS AFFECTED NO
PAX COMFORT AFFECTED NO POTENTIAL AD NO
RELIABILITY AFFECTED NO STRUCTURAL LIFE EXTENSION NO
LIFE LIMIT NO LINE MAINTENANCE AFFECTED NO NOTE: Service Bulletin must be accomplished.
D. MAINTENANCE CONFIGURATION
A350
SERVICE BULLETIN
SUMMARY REV 00 Sep 30/24 A350-32-P057 Page 3 No specific aircraft maintenance configuration required.
E. MATERIAL PRICE INFORMATION
(1) Inspection of the PN and Serial Number (SN) on the NLG Lower Torque Link
(a) T ask set A350-A-32-XX-P057-01000-93BA-A Inspection of the PN and SN on the NLG Lower T orque Link No material
(2) Depending on the Inspection Result, Replace the NLG Lower Torque Link
(a) T ask set A350-A-32-XX-P057-01000-93AA-A Depending on the Inspection Result, Replace the NLG Lower T orque Link No material F. APPLICABILITY This Service Bulletin is applicable to this (these) operator(s):
AAR AFL AFR AIC BAW CAL CCA CES CPA CSC CSN DAL DLH EDW ETD ETH EVE FBU FIN FJI
FWI GAF HVN IBE ITY JAL KAL KAY MAS MAU PAL QTR SAS SIA SJX SWR THA THY UAE VIR WFL G. CONCURRENT REQUIREMENTS None H. NATURE OF THE WORK
(1) Inspection of the PN and Serial Number (SN) on the NLG Lower Torque Link
(a) T ask set A350-A-32-XX-P057-01000-93BA-A Inspection of the PN and SN on the NLG Lower T orque Link
AIRCRAFT NO
EQUIPMENT YES
(2) Depending on the Inspection Result, Replace the NLG Lower Torque Link
(a) T ask set A350-A-32-XX-P057-01000-93AA-A Depending on the Inspection Result, Replace the NLG Lower T orque Link
AIRCRAFT NO
EQUIPMENT YES I. MANPOWER
(1) Inspection of the PN and Serial Number (SN) on the NLG Lower Torque Link
(a) T ask set A350-A-32-XX-P057-01000-93BA-A Inspection of the PN and SN on the NLG Lower T orque Link
MANPOWER TOTAL MAN-HOURS 0.75 h ELAPSED TIME (HOURS) 0.75 h
(2) Depending on the Inspection Result, Replace the NLG Lower Torque Link
(a) T ask set A350-A-32-XX-P057-01000-93AA-A Depending on the Inspection Result, Replace the NLG Lower T orque Link
MANPOWER TOTAL MAN-HOURS 8.00 h
A350
SERVICE BULLETIN
SUMMARY REV 00 Sep 30/24 A350-32-P057 Page 4
MANPOWER ELAPSED TIME (HOURS) 4.00 h
A350
SERVICE BULLETIN
SUMMARY Figure ICN-A350-A-32XXP057-A-FAPE3-07KQ4-A-001-01 Fig.SA Sol.AA SHEET 1/1 REV 00 Sep 30/24 A350-32-P057General Overview Page 5 J. GENERAL OVERVIEW
CONF ALL Z711 A A
INSPECTION OF THE PART NUMBER (PN)
AND SERIAL NUMBER (SN) ON THE
NOSE LANDING GEAR (NLG) 5011GN
LOWER TORQUE LINK ICN-A350-A-32XXP057-A-FAPE3-07KQ4-A-001-01
A350
SERVICE BULLETIN REV 00 Sep 30/24 A350-32-P057 Page 6 ATA SYSTEM: 32 TITLE: LANDING GEAR - NOSE LANDING GEAR (NLG) - LOWER TORQUE
LINKS MISSING BRIGHT SHOT PEENING
1. PLANNING INFORMATION A. APPLICABILITY
(1) Models ON A/C 0065, 0071, 0088, 0102, 0110, 0118, 0125, 0141, 0161, 0169, 0188, 0206, 0215, 0225, 0229, 0233, 0241, 0252, 0258, 0262, 0266, 0274, 0286, 0290, 0296, 0298, 0306, 0315, 0319, 0326, 0330, 0332, 0336, 0340, 0342, 0346, 0350, 0356, 0362, 0368, 0372, 0374, 0380, 0382, 0386, 0388, 0399, 0402, 0409, 0415, 0420, 0424, 0426, 0430, 0432, 0434, 0438, 0440, 0444, 0446, 0473, 0482, 0490, 0492, 0495, 0503, 0507, 0509, 0533, 0539, 0547, 0560, 0563, 0584, 0600, 0605, 0609, 0610, 0617, 0623, 0628, 0635, 0639, 0647, 0652, 0655, 0662, 0670, 0676, 0679, 0683, 0686, 0691, 0702, 0710, 0717, 0719, 0723, 0729, 0730, 0733, 0736, 0740, 0743, 0751, 0761 350-1041 ON A/C 0005-0058, 0060-0064, 0066-0070, 0072-0087, 0089-0101, 0103-0107, 0109, 0111- 0117, 0119-0124, 0126-0130, 0132-0138, 0140, 0142-0151, 0153-0155, 0157-0160, 0162- 0165, 0167, 0168, 0170, 0172-0187, 0189-0193, 0195-0205, 0207-0214, 0216-0221, 0223, 0224, 0226-0228, 0230-0232, 0234-0240, 0243-0251, 0254-0257, 0259-0261, 0263-0265, 0267-0273, 0276-0285, 0287, 0289, 0291-0295, 0297, 0299-0303, 0305, 0307-0314, 0316, 0318, 0320-0325, 0327-0329, 0331, 0333-0335, 0337-0339, 0341, 0343-0345, 0347-0349, 0351, 0352, 0354, 0355, 0357-0359, 0363-0366, 0369-0371, 0373, 0375, 0376, 0378, 0379, 0381, 0383, 0385, 0387, 0389-0398, 0400, 0401, 0403-0408, 0410-0414, 0416-0419, 0421- 0423, 0425, 0427-0429, 0431, 0433, 0435-0437, 0439, 0441-0443, 0445, 0447-0449, 0451- 0455, 0457-0460, 0462-0466, 0468-0472, 0474-0476, 0478-0481, 0483-0485, 0487-0489, 0491, 0493, 0494, 0496, 0497, 0499, 0500, 0502, 0504-0506, 0510, 0512, 0516, 0517, 0520, 0524, 0526, 0528, 0530, 0531, 0535-0537, 0540-0546, 0548-0552, 0554, 0556-0559, 0561, 0562, 0564, 0565, 0567-0583, 0585, 0587-0599, 0602-0604, 0607, 0611-0616, 0618, 0619, 0621, 0622, 0624-0627, 0629-0634, 0636-0638, 0640-0646, 0648-0651, 0653, 0654, 0656- 0661, 0663-0669, 0671-0675, 0677, 0678, 0680-0682, 0684, 0685, 0687-0690, 0692-0699, 0703-0706, 0708, 0709, 0711-0716, 0718, 0720-0722, 0724-0727, 0731, 0732, 0734, 0735, 0737-0739, 0741, 0742, 0745-0750, 0752, 0753, 0755 350-941
CONF ALL
(2) Applicability by MSN 0005-0058 0060-0107 0109-0130 0132-0138 0140-0151 0153-0155 0157-0165 0167- 0170 0172-0193 0195-0221 0223-0241 0243-0252 0254-0274 0276-0287 0289-0303 0305-0316 0318-0352 0354-0359 0362-0366 0368-0376 0378-0383 0385-0449 0451- 0455 0457-0460 0462-0466 0468-0476 0478-0485 0487-0497 0499 0500 0502-0507 0509 0510 0512 0516 0517 0520 0524 0526 0528 0530 0531 0533 0535-0537 0539- 0552 0554 0556-0565 0567-0585 0587-0600 0602-0605 0607 0609-0619 0621-0699 0702-0706 0708-0727 0729-0743 0745-0753 0755 0761
(3) MSN by configuration
MSN CONFIGURATION 0005 0006 0007 0008 0009 0010 0011 0012 0013 0014 0015 0016 0017 0018 0019 0020 0021 0022 0023 0024 0025 0026 0027 0028 0029 0030 0031 0032 0033 0034 0035 0036 0037 0038 0039 0040 0041 0042 0043 0044 0045 0046 0047 0048 0049 0050 0051 0052 0053 0054 0055 0056 0057 0058 0060 001
A350
SERVICE BULLETIN REV 00 Sep 30/24 A350-32-P057 Page 7
MSN CONFIGURATION 0061 0062 0063 0064 0065 0066 0067 0068 0069 0070 0071 0072 0073 0074 0075 0076 0077 0078 0079 0080 0081 0082 0083 0084 0085 0086 0087 0088 0089 0090 0091 0092 0093 0094 0095 0096 0097 0098 0099 0100 0101 0102 0103 0104 0105 0106 0107 0109 0110 0111 0112 0113 0114 0115 0116 0117 0118 0119 0120 0121 0122 0123 0124 0125 0126 0127 0128 0129 0130 0132 0133 0134 0135 0136 0137 0138 0140 0141 0142 0143 0144 0145 0146 0147 0148 0149 0150 0151 0153 0154 0155 0157 0158 0159 0160 0161 0162 0163 0164 0165 0167 0168 0169 0170 0172 0173 0174 0175 0176 0177 0178 0179 0180 0181 0182 0183 0184 0185 0186 0187 0188 0189 0190 0191 0192 0193 0195 0196 0197 0198 0199 0200 0201 0202 0203 0204 0205 0206 0207 0208 0209 0210 0211 0212 0213 0214 0215 0216 0217 0218 0219 0220 0221 0223 0224 0225 0226 0227 0228 0229 0230 0231 0232 0233 0234 0235 0236 0237 0238 0239 0240 0241 0243 0244 0245 0246 0247 0248 0249 0250 0251 0252 0254 0255 0256 0257 0258 0259 0260 0261 0262 0263 0264 0265 0266 0267 0268 0269 0270 0271 0272 0273 0274 0276 0277 0278 0279 0280 0281 0282 0283 0284 0285 0286 0287 0289 0290 0291 0292 0293 0294 0295 0296 0297 0298 0299 0300 0301 0302 0303 0305 0306 0307 0308 0309 0310 0311 0312 0313 0314 0315 0316 0318 0319 0320 0321 0322 0323 0324 0325 0326 0327 0328 0329 0330 0331 0332 0333 0334 0335 0336 0337 0338 0339 0340 0341 0342 0343 0344 0345 0346 0347 0348 0349 0350 0351 0352 0354 0355 0356 0357 0358 0359 0362 0363 0364 0365 0366 0368 0369 0370 0371 0372 0373 0374 0375 0376 0378 0379 0380 0381 0382 0383 0385 0386 0387 0388 0389 0390 0391 0392 0393 0394 0395 0396 0397 0398 0399 0400 0401 0402 0403 0404 0405 0406 0407 0408 0409 0410 0411 0412 0413 0414 0415 0416 0417 0418 0419 0420 0421 0422 0423 0424 0425 0426 0427 0428 0429 0430 0431 0432 0433 0434 0435 0436 0437 0438 0439 0440 0441 0442 0443 0444 0445 0446 0447 0448 0449 0451 0452 0453 0454 0455 0457 0458 0459 0460 0462 0463 0464 0465 0466 0468 0469 0470 0471 0472 0473 0474 0475 0476 0478 0479 0480 0481 0482 0483 0484 0485 0487 0488 0489 0490 0491 0492 0493 0494 0495 0496 0497 0499 0500 0502 0503 0504 0505 0506 0507 0509 0510 0512 0516 0517 0520 0524 0526 0528 0530 0531 0533 0535 0536 0537 0539 0540 0541 0542 0543 0544 0545 0546 0547 0548 0549 0550 0551 0552 0554 0556 0557 0558 0559 0560 0561 0562 0563 0564 0565 0567 0568 0569 0570 0571 0572 0573 0574 0575 0576 0577 0578 0579 0580 0581 0582 0583 0584 0585 0587 0588 0589 0590 0591 0592 0593 0594 0595 0596 0597 0598 0599 0600 0602 0603 0604 0605 0607 0609 0610 0611 0612 0613 0614 0615 0616 0617 0618 0619 0621 0622 0623 0624 0625 0626 0627 0628 0629 0630 0631 0632 0633 0634 0635 0636 0637 0638 0639 0640 0641 0642 0643 0644 0645 0646 0647 0648 0649 0650 0651 0652 0653 0654 0655 0656 0657 0658 0659 0660 0661 0662 0663 0664 0665 0666 0667 0668 0669 0670 0671 0672 0673 0674 0675 0676 0677 0678 0679 0680 0681 0682 0683 0684 0685 0686 0687 0688 0689 0690 0691 0692 0693 0694 0695 0696 0697 0698 0699 0702 0703 0704 0705 0706 0708 0709 0710 0711 0712 0713 0714 0715 0716 0717 0718 0719 0720 0721
A350
SERVICE BULLETIN REV 00 Sep 30/24 A350-32-P057 Page 8
MSN CONFIGURATION 0722 0723 0724 0725 0726 0727 0729 0730 0731 0732 0733 0734 0735 0736 0737 0738 0739 0740 0741 0742 0743 0745 0746 0747 0748 0749 0750 0751 0752 0753 0755 0761
(4) Configuration definition Configuration 001 CONF 001 is applicable for all the aircraft affected by this Service Bulletin as a standard configuration.
B. CONCURRENT REQUIREMENTS None C. REASON
(1) History During initial production of the Entry Into Service (EIS) standard NLG, some lower torque links (Part Number (PN) 5035-0401) were manufactured without bright shot peening. The omission of bright shot peening may reduce the life limitation of the component, depending on which aircraft weight variant and NLG standard the component is installed on.
(2) Objective/Action The objective of this Inspection Service Bulletin (ISB) is to give the required information for the operators to be able to determine for each affected lower torque link the new life limitation.
(3) Advantages The accomplishment of this ISB ensures that the right life for the affected torque link and therefore ensure to not exceed the correct life limitation.
(4) Operational/Maintenance Consequences None D. DESCRIPTION T o accomplish this Service Bulletin it is necessary to:
(1) Inspection of the PN and Serial Number (SN) on the NLG Lower Torque Link
(a) T ask set A350-A-32-XX-P057-01000-93BA-A Inspection of the PN and SN on the NLG Lower T orque Link 1 Inspect the PN and SN on the NLG Lower T orque Link
(2) Depending on the Inspection Result, Replace the NLG Lower Torque Link
(a) T ask set A350-A-32-XX-P057-01000-93AA-A Depending on the Inspection Result, Replace the NLG Lower T orque Link 1 Replace the NLG Lower T orque Link E. COMPLIANCE
(1) Classification MANDATORY: Service Bulletin must be accomplished.
A350
SERVICE BULLETIN REV 00 Sep 30/24 A350-32-P057 Page 9
(2) Accomplishment Timescale Accomplishment of this Service Bulletin must be done within a maximum of 30 days from the initial issue date of the ISB.
This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Union Aviation Safety Agency (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds and/or interval given above but reference should be made to the AD for confirmation of the mandated accomplishment timescale.
F. APPROVAL The technical content of this document is approved under the authority of the Design Organisation Approval ref. EASA.21J.031.
If an aircraft listed in the applicability has a modification or repair embodied that is not of AIRBUS origin, and which affects the content of this Service Bulletin, the operator is responsible for obtaining approval by its airworthiness authority for any adaptation necessary before incorporation of the Service Bulletin.
G. MANPOWER The manpower estimates given in this Service Bulletin are based on the direct labor cost to do the work. These estimates assume that the work will be done by experienced personnel, and may need to be revised upwards to suit operator’s circumstances. The estimates do not include the time to prepare, plan or inspect the work. Manufacture and procurement of parts and tools, drying times for paints, sealants, etc., and general administration work are also not included.
(1) Inspection of the PN and Serial Number (SN) on the NLG Lower Torque Link
(a) T ask set A350-A-32-XX-P057-01000-93BA-A Inspection of the PN and SN on the NLG Lower T orque Link
PREPARATION Job Set-up 0.25 h
PROCEDURE Inspect the PN and SN on the NLG Lower T orque Link 0.25 h
PREPARATION FOR TEST None TEST None
CLOSE-UP Close-up 0.25 h TOTAL MAN-HOURS 0.75 h ELAPSED TIME (HOURS) 0.75 h
(2) Depending on the Inspection Result, Replace the NLG Lower Torque Link
(a) T ask set A350-A-32-XX-P057-01000-93AA-A Depending on the Inspection Result, Replace the NLG Lower T orque Link
PREPARATION Job Set-up 1.00 h
PROCEDURE Replace the NLG Lower T orque Link 2.00 h
A350
SERVICE BULLETIN REV 00 Sep 30/24 A350-32-P057 Page 10
PREPARATION FOR TEST None TEST Clearance Check 4.00 h
CLOSE-UP Close-up 1.00 h TOTAL MAN-HOURS 8.00 h ELAPSED TIME (HOURS) 4.00 h H. WEIGHT AND BALANCE Not changed I. ELECTRICAL LOAD DATA Not changed J. REFERENCES
(1) Inspection of the PN and Serial Number (SN) on the NLG Lower Torque Link
(a) T ask set A350-A-32-XX-P057-01000-93BA-A Inspection of the PN and SN on the NLG Lower T orque Link
AIRWORTHINESS LIMITATION SECTION (ALS) Part 1
ELECTRICAL STANDARD PRACTICES (ESP) A350-A-20-55-XX-01ZZZ-042Z-A
INTRODUCTION (INTRO) A350-A-00-61-04-11ZZZ-018Z-D
MAINTENANCE PROCEDURE (MP) A350-A-24-41-XX-00ZZZ-170Z-A
SYSTEM DESCRIPTION (SD) A350-A-06-3X-XX-01ZZZ-04CZ-A
(2) Depending on the Inspection Result, Replace the NLG Lower Torque Link
(a) T ask set A350-A-32-XX-P057-01000-93AA-A Depending on the Inspection Result, Replace the NLG Lower T orque Link
ELECTRICAL STANDARD PRACTICES (ESP) A350-A-20-55-XX-01ZZZ-042Z-A
INTRODUCTION (INTRO) A350-A-00-61-04-11ZZZ-018Z-D
MAINTENANCE PROCEDURE (MP) A350-A-24-41-XX-00ZZZ-170Z-A A350-A-32-21-69-00ZZZ-520Z-A A350-A-32-21-69-00ZZZ-720Z-A
A350
SERVICE BULLETIN REV 00 Sep 30/24 A350-32-P057 Page 11
SYSTEM DESCRIPTION (SD) A350-A-06-3X-XX-01ZZZ-04CZ-A K. PUBLICATION AFFECTED None L. INDUSTRY SUPPORT INFORMATION This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign. For detailed support, please refer to the related RIL V32M24001635.
For the organization of this retrofit, you are kindly requested to contact AIRBUS retrofit management department: monitored.retrofit@airbus.com.
A350
SERVICE BULLETIN REV 00 Sep 30/24 A350-32-P057 Page 12
2. MATERIAL INFORMATION A. MATERIAL APPLICABILITY No material for task set A350-A-32-XX-P057-01000-93BA-A Inspection of the PN and SN on the NLG Lower Torque Link Material for task set A350-A-32-XX-P057-01000-93AA-A Depending on the Inspection Result, Replace the NLG Lower Torque Link
MATERIAL QTY SEE NOTES Referenced tools See SB Referenced consumables See SB Referenced parts See SB B. TOOLING Referenced tools for task set A350-A-32-XX-P057-01000-93AA-A Depending on the Inspection Result, Replace the NLG Lower Torque Link T o accomplish this Service Bulletin it is necessary to use the tools listed in:
Ref. MP A350-A-32-21-69-00ZZZ-520Z-A Ref. MP A350-A-32-21-69-00ZZZ-720Z-A C. CONSUMABLES Referenced consumables for task set A350-A-32-XX-P057-01000-93AA-A Depending on the Inspection Result, Replace the NLG Lower Torque Link T o accomplish this Service Bulletin it is necessary to use the consumable materials listed in:
Ref. MP A350-A-32-21-69-00ZZZ-720Z-A D. LIST OF NEW PARTS Referenced parts for task set A350-A-32-XX-P057-01000-93AA-A Depending on the Inspection Result, Replace the NLG Lower Torque Link T o accomplish this Service Bulletin it is necessary to use the expendable parts listed in:
Ref. MP A350-A-32-21-69-00ZZZ-720Z-A E. LIST OF EXISTING PARTS No parts