# Airbus Service Bulletin A340-57-4148 Copy: No revision named ("A340-57-4148 R00"), 88 pages: PDF https://openairdocs.org/files/sha256/73/b0/73b0bf28a4d80e74dbb0da491cc0116055553f3038c72ba749e1871a048b5659; text https://openairdocs.org/service-documents/airbus/a340-57-4148/file/73b0bf28a4d8.md. Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2019-0320, the docket of AD 2019-17-05. Not covered by OpenAirDocs’ CC0 dedication. ## Details - Manufacturer: [Airbus](https://openairdocs.org/service-documents/airbus.md) - Type: Service bulletin (Service Bulletin) - Number: A340-57-4148 - Page: https://openairdocs.org/service-documents/airbus/a340-57-4148 ## Text (88 pages) Rights: © Airbus S.A.S. Filed by the FAA in regulations.gov docket FAA-2019-0320, the docket of AD 2019-17-05. Not covered by OpenAirDocs’ CC0 dedication. Each page's text from the PDF; open the PDF at a page with #page=N. ### Page 1 @A340 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 This summary is for information only and is not approved for modification of the aircraft. MANDATORY MANDATORY MANDATORY ATA SYSTEM: 57 TITLE: WINGS-LEADING EDGE AND LEADING EDGE DEVICES-INSPECTION OF SLAT TRACKS NUMBER 10 REFERENCES **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Some slat track references were implemented as spares in Illustrated Parts Catalog (IPC) in June 2010 when in fact those references for slat tracks No. 10 are not able to sustain ultimate load for some weight variants. IPC documents review and correction is still ongoing. AIRBUS is aiming to finalize the correction in October 2018. Even investigation is demonstrating that impacted references were never delivered as spare part, possible slat track swap between aircraft cannot be excluded due to wrong IPC data. The aim of this inspection is to identify if affected part numbers have been installed. In case of wrong part installed, the slat track will have to be replaced according to the accomplishment timescale. If no affected part number is installed, no further action is requested. Accomplishment of this Service Bulletin will contribute to make sure that the slat tracks installed can sustain the ultimate loads corresponding to the weight variant of the aircraft. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE MANDATORY (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO LROPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1) : Service Bulletin must be accomplished. DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 2 @A340 SERVICE BULLETIN SUMMARY MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Component COMPB01 2 See SB Nuts, cotter pins, bearing Component COMPB02 2 See SB Nuts, cotter pins Component COMPB03 2 See SB Track assy-No 10 EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) : 06Y 14S 17M 26L 36L 39N 65W 78U 83V ABB ABD AFR AIB ARG AXY BEL BOE CAL D2F DLH EDW F2I GAF HFM HFY IRM KMF MAU MDG MRJ PAL PUE QQE ROI S3R SAA SAS SLM SWR SYR THT THY U6A CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU 57.40.00.022 OEB None AOT None SIL None ISI 00.00.00285 00.05.00003 11.00.00002 LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER Operator Information Transmission (OIT) No. 999-0058/16 OTHER OIT No. 999-0066/17 NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO MANPOWER Task 574148-832-895-001: Special Detailed Inspection of the Slat Tracks No. 10 References TOTAL MANHOURS 6.50 ELAPSED TIME (HOURS) 1.25 Task 574148-833-895-001: Replacement of the Slat Track(s) No. 10 TOTAL MANHOURS 8.00 ELAPSED TIME (HOURS) 4.00 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 3 @A340 SERVICE BULLETIN SUMMARY APPENDICES Appendix 01 - Inspection Report Appendix 02 - Manpower Gantt Chart DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 4 @A340 SERVICE BULLETIN SUMMARY **CONF ALL SLAT 4 SLAT TRACK No 9 A LH SHOWN RH SYMMETRICAL SLAT TRACK No 10 TO BE INSPECTED Z622 Z522A A F_SB_574148_7_SAAA_01_00 Figure A-USAAA - Sheet 01 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 5 @A340 SERVICE BULLETIN AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE T e l:( 3 3 )56 19 33 33 3 Telex : AIRBU 530526F F a x:( 3 3 )56 19 34 25 1 MANDATORY MANDATORY MANDATORY ATA SYSTEM: 57 TITLE: WINGS-LEADING EDGE AND LEADING EDGE DEVICES-INSPECTION OF SLAT TRACKS NUMBER 10 REFERENCES MODIFICATION No.: None This document contains AIRBUS PROPRIETARY INFORMATION and shall at all times remain the property of AIRBUS; no intellectual property right or licence is granted by AIRBUS in connection with any information contained in it. It is delivered on the express condition that said document and the information contained in it shall be treated as confidential, shall not be used for any purpose other than that for which it is hereby delivered. It shall not be disclosed in whole or in part to third parties and shall not be duplicated in any manner (except for the purposes of performing the tasks described hereunder and provided that any recipient of such document shall comply with the conditions herein), without AIRBUS prior written consent. 1. PLANNING INFORMATION **CONF ALL A. EFFECTIVITY (1) Models 340-213 340-312 340-313 (2) Effectivity by MSN 0117 0123 0126 0128 0135 0139 0149 0152 0158 0163-0164 0166-0168 0170 0174-0175 0179-0180 0185-0186 0190 0192-0194 0197 0199 0201-0202 0204 0207-0208 0210 0212-0215 0217 0221 0233 0236-0237 0242-0243 0245-0246 0252 0257 0260 0264 0268 0270 0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325 0327 0329 0331-0332 0335 0347 0352 0354-0355 0367 0373-0374 0377-0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413 0415 0424 0430 0433-0435 0438 0446-0447 0450 0459 0467 0470 0474 0483 0528 0538 0541 0544-0546 0554 0556 0559 0561-0562 0582 0585 0590 0598 0643 0646 0651 0668 0793 0800 0835 0844 0921 0938 0955 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 1 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 6 @A340 SERVICE BULLETIN (3) Effectivity by Operator The Operator/MSN relationship is provided for information only and is correct at the time of issue in accordance with the information available to AIRBUS. Any future changes resulting from transfer of an aircraft from one operator to another will not be reflected in this list unless the Service Bulletin is revised for another reason. OPERATOR MSN 06Y 0139 0149 14S 0152 17M 0955 26L 0217 0221 0329 36L 0406 39N 0168 0174 65W 0208 78U 0175 0179 83V 0280 ABB 0835 0844 0921 0938 ABD 0210 AFR 0186 0207 0245 0246 0260 0377 AIB 0192 0243 0264 ARG 0123 0126 0170 0193 AXY 0374 BEL 0335 0354 BOE 0554 CAL 0402 0411 0415 0433 0541 D2F 0128 DLH 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327 0347 0352 0379 0390 0434 0447 EDW 0556 0559 0561 0562 F2I 0117 0214 0237 0307 0310 GAF 0274 0355 HFM 0163 0166 0185 0236 0367 0483 HFY 0190 0202 IRM 0164 0282 0292 KMF 0278 0318 0387 MAU 0194 0268 0793 0800 MDG 0319 MRJ 0257 PAL 0302 0332 0459 0474 PUE 0212 0215 0399 QQE 0528 ROI 0199 0201 S3R 0204 SAA 0197 0378 0544 0582 0590 0643 0646 0651 SAS 0167 0413 0424 0430 0435 0450 0467 0470 SLM 0242 SWR 0538 0545 0546 0585 0598 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 2 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 7 @A340 SERVICE BULLETIN OPERATOR MSN SYR 0381 THT 0385 0395 0438 0446 0668 THY 0180 0270 0331 U6A 0373 (4) Configuration by MSN MSN CONFIGURATION 0117 0123 0126 0128 0135 0139 0149 0152 0158 0163 0164 0166 0167 0168 0170 0174 0175 0179 0180 0185 0186 0190 0192 0193 0194 0197 0199 0201 0202 0204 0207 0208 0210 0212 0213 0214 0215 0217 0221 0233 0236 0237 0242 0243 0245 0246 0252 0257 0260 0264 0268 0270 0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318 0319 0321 0325 0327 0329 0331 0332 0335 0347 0352 0354 0355 0367 0373 0374 0377 0378 0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413 0415 0424 0430 0433 0434 0435 0438 0446 0447 0450 0459 0467 0470 0474 0483 0528 0538 0541 0544 0545 0546 0554 0556 0559 0561 0562 0582 0585 0590 0598 0643 0646 0651 0668 0793 0800 0835 0844 0921 0938 0955 001 (5) Configuration definition **CONF 001 Config. 001 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Component COMPB01 2 Component COMPB02 2 Component COMPB03 2 Consumable CMLB01 1 B. CONCURRENT REQUIREMENTS None C. REASON (1) History Some slat track references were implemented as spares in Illustrated Parts Catalog (IPC) in June 2010 when in fact those references for slat tracks No. 10 are not able to sustain ultimate load for some weight variants. IPC documents review and correction is still ongoing. AIRBUS is aiming to finalize the correction in October 2018. Even investigation is demonstrating that impacted references were never delivered as spare part, possible slat track swap between aircraft cannot be excluded due to wrong IPC data. DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 3 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 8 @A340 SERVICE BULLETIN (2) Objective/Action The aim of this inspection is to identify if affected part numbers have been installed. In case of wrong part installed, the slat track will have to be replaced according to the accomplishment timescale. If no affected part number is installed, no further action is requested. (3) Advantages Accomplishment of this Service Bulletin will contribute to make sure that the slat tracks installed can sustain the ultimate loads corresponding to the weight variant of the aircraft. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 574148-832-895-001: Special Detailed Inspection of the Slat Tracks No. 10 References (1) Inspect the Slat Track No. 10 Identification Plate on the LH Side (2) Inspect the Slat Track No. 10 Identification Plate on the RH Side (3) Depending on the Inspection Results, Remove the Link Parts between the Slat 4 and the Slat Track No. 10 on the LH Side (4) Depending on the Inspection Results, Remove the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side (5) Depending on the Inspection Results, Do a Detailed Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the LH Side (6) Depending on the Inspection Results, Do a Detailed Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the RH Side (7) Depending on the Inspection Results, Do an HFEC Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the LH Side (8) Depending on the Inspection Results, Do an HFEC Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the RH Side (9) Depending on the Inspection Results, Install the Link Parts between the Slat 4 and the Slat Track No. 10 on the LH Side (10) Depending on the Inspection Results, Install the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side (11) Depending on the Inspection Results, Identify the Slat Track No. 10 on the LH Side DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 4 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 9 @A340 SERVICE BULLETIN (12) Depending on the Inspection Results, Identify the Slat Track No. 10 on the RH Side Task 574148-833-895-001: Replacement of the Slat Track(s) No. 10 (1) Depending on the Inspection Results, Replace the Slat Track No. 10 on the LH Side (2) Depending on the Inspection Results, Replace the Slat Track No. 10 on the RH Side E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale This Service Bulletin has been classified Mandatory. It is expected that an Airworthiness Directive (AD) published by the European Av iation Safety Agenc y (EASA) will be issued to confirm this classification. It is anticipated that the AD will confirm the thresholds given but reference should be made to the AD for confirmation of the mandated accomplishment timescale. Table 1, Config 001 - Special Detailed Inspection of the Slat Track No. 10 Reference on the LH Side Condition Action Compliance time Repetitive interval All aircraft Inspect the slat track No. 10 identification plate in accordance with TASK 574148-832-895-001 Within 24 months from the issuance date of this Service Bulletin None Remove the link parts between the slat 4 and the slat track No. 10 in accordance with SUBTASK 574148-020-401-001 And Before next flight None If the identification plate is missing or is not readable Measure the aft lug upper thickness of the slat track No. 10 in accordance with SUBTASK 574148-210-401-001 Before next flight None Do a detailed inspection in the upper area of the aft lug of the slat track No. 10 in accordance with SUBTASK 574148-220-401-001 And Before next flight None If the dimension measured is equal to 10.80 mm (0.425 in.) Do an HFEC inspection in the upper area of the aft lug of the slat track No. 10 in accordance with SUBTASK 574148-250-401-001 Before next flight None DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 5 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 10 @A340 SERVICE BULLETIN Table 1, Config 001 - Special Detailed Inspection of the Slat Track No. 10 Reference on the LH Side Condition Action Compliance time Repetitive interval Upload the inspection report And Before next flight None Contact AIRBUS for slat track spare preparation And Before next flight None If the dimension measured is equal to 10.80 mm (0.425 in.) and crack is found Replace the affected slat track No. 10 by a new part number F5746412700200 in accordance with TASK 574148-833-895-001 Before next flight None Install the link parts between the slat 4 and the slat track No. 10 in accordance with SUBTASK 574148-420-401-001 And Before next flight None Identify the slat track No. 10 in accordance with SUBTASK 574148-831-401-001 And Before next flight None Upload the inspection report And Before next flight None Contact AIRBUS for slat track spare preparation And Before next flight None If the dimension measured is equal to 10.80 mm (0.425 in.) and no crack is found Replace the affected slat track No. 10 by a new part number F5746412700200 in accordance with TASK 574148-833-895-001 Within 3 months from the inspection date None Install the link parts between the slat 4 and the slat track No. 10 in accordance with SUBTASK 574148-420-401-001 And Before next flight None Identify the slat track No. 10 in accordance with SUBTASK 574148-831-401-001 And Before next flight None If the dimension measured is not equal to 10.80 mm (0.425 in.) No further action None None If the identification plate is not missing and is readable Inspect the slat track No. 10 part number in accordance with SUBTASK 574148-210-401-001 Before next flight None DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 6 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 11 @A340 SERVICE BULLETIN Table 1, Config 001 - Special Detailed Inspection of the Slat Track No. 10 Reference on the LH Side Condition Action Compliance time Repetitive interval Remove the link parts between the slat 4 and the slat track No. 10 in accordance with SUBTASK 574148-020-401-001 And Before next flight None Do a detailed inspection in the upper area of the aft lug of the slat track No. 10 in accordance with SUBTASK 574148-220-401-001 And Before next flight None If aircraft is equipped with part number F5746411000000 or F5746411000200 Do an HFEC inspection in the upper area of the aft lug of the slat track No. 10 in accordance with SUBTASK 574148-250-401-001 Before next flight None Upload the inspection report And Before next flight None Contact AIRBUS for slat track spare preparation And Before next flight None If aircraft is equipped with part number F5746411000000 or F5746411000200, and crack is found Replace the affected slat track No. 10 by a new part number F5746412700200 in accordance with TASK 574148-833-895-001 Before next flight None Install the link parts between the slat 4 and the slat track No. 10 in accordance with SUBTASK 574148-420-401-001 And Before next flight None Upload the inspection report And Before next flight None Contact AIRBUS for slat track spare preparation And Before next flight None If aircraft is equipped with part number F5746411000000 or F5746411000200, and no crack is found Replace the affected slat track No. 10 by a new part number F5746412700200 in accordance with TASK 574148-833-895-001 Within 3 months from the inspection date None If aircraft is not equipped with part number F5746411000000 or F5746411000200 No further action None None DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 7 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 12 @A340 SERVICE BULLETIN Table 2, Config 001 - Special Detailed Inspection of the Slat Track No. 10 Reference on the RH Side Condition Action Compliance time Repetitive interval All aircraft Inspect the slat track No. 10 identification plate in accordance with TASK 574148-832-895-001 Within 24 months from the issuance date of this Service Bulletin None Remove the link parts between the slat 4 and the slat track No. 10 in accordance with SUBTASK 574148-020-402-001 And Before next flight None If the identification plate is missing or is not readable Measure the aft lug upper thickness of the slat track No. 10 in accordance with SUBTASK 574148-210-402-001 Before next flight None Do a detailed inspection in the upper area of the aft lug of the slat track No. 10 in accordance with SUBTASK 574148-220-402-001 And Before next flight None If the dimension measured is equal to 10.80 mm (0.425 in.) Do an HFEC inspection in the upper area of the aft lug of the slat track No. 10 in accordance with SUBTASK 574148-250-402-001 Before next flight None Upload the inspection report And Before next flight None Contact AIRBUS for slat track spare preparation And Before next flight None If the dimension measured is equal to 10.80 mm (0.425 in.) and crack is found Replace the affected slat track No. 10 by a new part number F5746412700200 in accordance with TASK 574148-833-895-001 Before next flight None Install the link parts between the slat 4 and the slat track No. 10 in accordance with SUBTASK 574148-420-402-001 And Before next flight None Identify the slat track No. 10 in accordance with SUBTASK 574148-831-402-001 And Before next flight None Upload the inspection report And Before next flight None Contact AIRBUS for slat track spare preparation And Before next flight None If the dimension measured is equal to 10.80 mm (0.425 in.) and no crack is found Replace the affected slat track No. 10 by a new part number F5746412700200 in accordance with TASK 574148-833-895-001 Within 3 months from the inspection date None DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 8 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 13 @A340 SERVICE BULLETIN Table 2, Config 001 - Special Detailed Inspection of the Slat Track No. 10 Reference on the RH Side Condition Action Compliance time Repetitive interval Install the link parts between the slat 4 and the slat track No. 10 in accordance with SUBTASK 574148-420-402-001 And Before next flight None Identify the slat track No. 10 in accordance with SUBTASK 574148-831-402-001 And Before next flight None If the dimension measured is not equal to 10.80 mm (0.425 in.) No further action None None If the identification plate is not missing or is readable Inspect the slat track No. 10 part number in accordance with SUBTASK 574148-210-402-001 Before next flight None Remove the link parts between the slat 4 and the slat track No. 10 in accordance with SUBTASK 574148-020-402-001 And Before next flight None Do a detailed inspection in the upper area of the aft lug of the slat track No. 10 in accordance with SUBTASK 574148-220-402-001 And Before next flight None If aircraft is equipped with part number F5746411000000 or F5746411000200 Do an HFEC inspection in the upper area of the aft lug of the slat track No. 10 in accordance with SUBTASK 574148-250-402-001 Before next flight None Upload the inspection report And Before next flight None Contact AIRBUS for slat track spare preparation And Before next flight None If aircraft is equipped with part number F5746411000000 or F5746411000200, and crack is found Replace the affected slat track No. 10 by a new part number F5746412700200 in accordance with TASK 574148-833-895-001 Before next flight None DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 9 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 14 @A340 SERVICE BULLETIN Table 2, Config 001 - Special Detailed Inspection of the Slat Track No. 10 Reference on the RH Side Condition Action Compliance time Repetitive interval Install the link parts between the slat 4 and the slat track No. 10 in accordance with SUBTASK 574148-420-402-001 And Before next flight None Upload the inspection report And Before next flight None Contact AIRBUS for slat track spare preparation And Before next flight None If aircraft is equipped with part number F5746411000000 or F5746411000200, and no crack is found Replace the affected slat track No. 10 by a new part number F5746412700200 in accordance with TASK 574148-833-895-001 Within 3 months from the inspection date None If aircraft is not equipped with part number F5746411000000 or F5746411000200 No further action None None F. APPROVAL The technical content of this document is approved under the authority of Design Organisation Approval No. EASA.21J.031. If an aircraft listed in the effectivity 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. NOTE : The minimum man-hours necessary to accomplish this Service Bulletin are those for the Inspection. Depending on the inspection result, additional man- hours can apply. Task 574148-832-895-001: Special Detailed Inspection of the Slat Tracks No. 10 References Get Access 0.50 On Aircraft DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 10 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 15 @A340 SERVICE BULLETIN Task 574148-832-895-001: Special Detailed Inspection of the Slat Tracks No. 10 References Inspect the Slat Track No. 10 Identification Plate on the LH Side 0.25 Inspect the Slat Track No. 10 Identification Plate on the RH Side 0.25 Depending on the Inspection Results, Remove the Link Parts between the Slat 4 and the Slat Track No. 10 on the LH Side 0.50 Depending on the Inspection Results, Remove the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side 0.50 Depending on the Inspection Results, Do a Detailed Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the LH Side 0.50 Depending on the Inspection Results, Do a Detailed Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the RH Side 0.50 Depending on the Inspection Results, Do an HFEC Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the LH Side 0.50 Depending on the Inspection Results, Do an HFEC Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the RH Side 0.50 Depending on the Inspection Results, Install the Link Parts between the Slat 4 and the Slat Track No. 10 on the LH Side 0.50 Depending on the Inspection Results, Install the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side 0.50 Depending on the Inspection Results, Identify the Slat Track No. 10 on the LH Side 0.50 Depending on the Inspection Results, Identify the Slat Track No. 10 on the RH Side 0.50 Close-Up 0.50 TOTAL MANHOURS 6.50 ELAPSED TIME (HOURS) 1.25 NOTE : For an explanation of the man-hours and elapsed time, refer to the Gantt Chart, Fig. A-UABAA given in Appendix 02. Task 574148-833-895-001: Replacement of the Slat Track(s) No. 10 Get Access 1.00 On Aircraft Depending on the Inspection Results, Replace the Slat Track No. 10 on the LH Side 3.00 Depending on the Inspection Results, Replace the Slat Track No. 10 on the RH Side 3.00 Close-Up 1.00 TOTAL MANHOURS 8.00 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 11 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 16 @A340 SERVICE BULLETIN Task 574148-833-895-001: Replacement of the Slat Track(s) No. 10 ELAPSED TIME (HOURS) 4.00 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES Aircraft Maintenance Manual (AMM) 06-20-00 12-34-24 20-21-11 27-80-00 27-84-69 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-55-00 Non Destructive Test Manual (NTM) 51-10-08 51-90-00 Process and Material Specification (PMS) Process and Material Specification (PMS) 01-06-13 Standards Manual (SM) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-75-12 K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 12 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 17 @A340 SERVICE BULLETIN 2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses For standard hardware the purchase order shall be addressed to AIRBUS. Quote the number of this Service Bulletin, the MSN and, if applicable the Retrofit Information Letter (RIL) reference. Please send your request to: Component COMPB01 Component COMPB02 AIRBUS Material, Logistics and Suppliers Standard Parts For ordering by internet: http://spares.airbus.com or vi a SPEC2000 For ordering by E-mail: ifd.spares@airbus.com Phone: +49 (0) 40 50 76 40 03 Customers with aircraft shown in the effectivity of this Service Bulletin should send a purchase order to AIRBUS. Quote the number of this Service Bulletin. The address is: Component COMPB03 AIRBUS Material, Logistics and Suppliers IFD - In Flight Desk Weg beim Jaeger 150 D-22335 HAMBURG GERMANY For ordering by internet: http://spares.airbus.com For ordering by fax: +49 40 50 76 4012 For ordering by E-mail: ifd.spares@airbus.com (2) Price and Availability Operator supplied AIRBUS parts required to accomplish this Service Bulletin are to be purchased by a spares purchase order. Operator supplied standard hardware parts, required to accomplish this Service Bulletin, are to be supplied from the operator’s stock. B. INDUSTRY SUPPORT INFORMATION In case of findings, AIRBUS will share the costs of accomplishment of this Service Bulletin by crediting the operator supplied AIRBUS parts for orders placed within 24 months after the initial issue date of the Service Bulletin. AIRBUS will not credit the man-hours indicated in this Service Bulletin. They remain at operator’s charge. This Service Bulletin is the subject of an AIRBUS monitored retrofit campaign. DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 13 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 18 @A340 SERVICE BULLETIN For the organization of this retrofit, you are kindly requested to contact AIRBUS retrofit management department: monitored.retrofit@airbus.com. C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Mineral Base Lubricating Oil - General and Water-Disp 03BDB9 As required Synthetic Oil Base Grease - General Purpose Clay Th 03GBB1 As required Coating - Flexible Structure 04QAB2 As required Polysulfide Sealant - General Purpose Brushable 06AAA1 As required Polysulfide Sealant - General Purpose Fillet 06AAB1 As required Polysulfide Sealant - Fuel Tank Brushable 06ABA1 As required Non Aqueous Cleaner - General 08BAA9 As required Paste Adhesive-Epoxy Potting Structure 13FBB2 As required Textile - Lint Free Cotton 14SBA1 As required (2) Components NOTE : To accomplish this Service Bulletin it is necessary to use the expendable parts listed in the subs equent referenced tasks: - AMM Task 27-84-69-400-801. Component COMPB01 ITEM NEW PART N˚ QTY (UM) KEYWORD ITEM OLD PART N˚ INT SEE NOTES 11 NSA5059C12 1 NUT 12 NSA5059C10 1 NUT 13 ABS0571-14W 1 BEARING 16 MS24665-376 2 PIN 18 NSA9117-22B 1 PLATE DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 14 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 19 @A340 SERVICE BULLETIN NOTE : If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. NOTE : The components listed above are only necessary if the identification plate is missing or is not readable, and no crack is found. The quantity of these items are to be ordered as required. NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. Component COMPB02 ITEM NEW PART N˚ QTY (UM) KEYWORD ITEM OLD PART N˚ INT SEE NOTES 11 NSA5059C12 1 NUT 12 NSA5059C10 2 NUT 16 MS24665-376 3 PIN NOTE : If you find part numbers of hardware components in the related kit(s) which you cannot identify in the LIST OF COMPONENTS of this Service Bulletin, refer to Standards Manual (SM). The SM will give you the correct part number to part number relationship. NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE : The components listed above are only necessary if the slat track No. 10 is replaced. The quantity of these items are to be ordered as required. Component COMPB03 ITEM NEW PART N˚ QTY (UM) KEYWORD ITEM OLD PART N˚ INT SEE NOTES 19 F5746412700200 1 TRACK NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE : The components listed above are only necessary if the slat track No. 10 is replaced. The quantity of these items are to be ordered as required. (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 15 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 20 @A340 SERVICE BULLETIN F. TOOLING (1) Tooling - Price and Availability None (2) Tools NOTE : To accomplish this Service Bulletin it is necessary to use the tools listed in the subsequent re ferenced tasks: - AMM Task 27-80-00-866-801 - AMM Task 27-84-69-000-801 - NTM 51-10-08 - NTM 51-90-00. (3) Special Tools None DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 16 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 21 @A340 SERVICE BULLETIN 3. ACCOMPLISHMENT INSTRUCTIONS Task 574148-832-895-001 - Special Detailed Insp ection of the Slat Tracks No. 10 References WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE) . WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC., AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00. NOTE : The accomplishment instructions of this Service Bulletin include procedures given in other documents or in other sections of the Service Bulletin. When the words ’refer to’ are used and the operator has a procedure accepted by the local authority he belongs to, the accepted alternative procedure can be used. When the words ’in accordance with’ are used then the given procedure must be followed. NOTE : The access and close-up instructions, not comprising return to service tests, in this Service Bulletin do not constitute or affect the technical intent of the Service Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or close-up steps to add flexibility to their maintenance operations as long as the technical intent of the Service Bulletin is met within the set parameters. NOTE : Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms. NOTE : This Service Bulletin contains the instructions for the on-aircraft maintenance necessary to ensure the continued airworthiness of the aircraft. For any deviations to the instructions, including RC paragraph contained herein, contact AIRBUS for further instructions and approval. NOTE : The purpose of flowcharts is to supplement the information given in the Procedure and Compliance paragraphs and not to serve as the primary source for tasks or compliance times given in this Service Bulletin. NOTE : This Service Bulletin is classified mandatory or expected to be classified mandatory by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these accomplishment instructions are Required for Compliance (RC) and must be done DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 17 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 22 @A340 SERVICE BULLETIN to comply with the AD. To allow more flexibility, the rule "refer to" and "in accordance with" will apply to these paragraphs 3.C. and 3.D. Other paragraphs are recommended and may be deviated from, done as part of other actions or done with accepted methods different from those given in the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can be put back into a serviceable condition. NOTE : Discarded parts must be managed at the operator’s discretion. Task Associated Data Zone 522 622 Manpower TOTAL MANHOURS 6.50 ELAPSED TIME (HOURS) 1.25 A. GENERAL (1) Subtask 574148-910-401-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 Task 20-21-11-911-801 Consumable Material List (CML) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-75-12 (a) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (b) If alternative and substitute fasteners have to be used, you must make sure that the associated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’ column. (c) Remove and install fasteners in accordance with SRM 51-42-00. (d) Get alternative and substitute fastener data in accordance with SRM 51-43-00. (e) To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-801. (f) Apply sealant in accordance with SRM 51-24-00. (g) For the specification of Material Numbers (Mat. No.) given in this Service Bulletin, refer to the Consumable Materials List (CML). DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 18 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 23 @A340 SERVICE BULLETIN (h) Renew the protective finish in accordance with SRM 51-75-12. (i) Tag all the parts you must remove and retain to make the subsequent installation easier. (j) Put all the retained hardware in identified plastic bags and attach the bags to the related unit. (k) If you find process and material specifications that you do not know in the design drawings, refer to the cross-reference list in the Process and Material Specification (PMS). (2) Subtask 574148-839-401-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION (1) Subtask 574148-941-401-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 Task 27-80-00-866-801 NOTE : For the basic Aircraft configuration, refer to AMM Chapter "Introduction - Aircraft status for maintenance" in Manual Front Matter section. (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. (b) Extend the slats, refer to AMM Task 27-80-00-866-801. (c) Put an access platform in position at zones 522 and 622. C. PROCEDURE (1) Subtask 574148-210-401-001 - Inspect the Slat Track No. 10 Identification Plate on the LH Side Work Zones and Access Panels Zone Access/Work location 522 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 19 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 24 @A340 SERVICE BULLETIN Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills NON SPECIFIC Material necessary to do the job Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner - General 08BAA9 As required Textile - Lint Free Cotton 14SBA1 As required References Fig. A-UFAAA Flowchart Sheet 01 Sheet 02 Sheet 03 Fig. A-UBAAA Inspection of the Identification Plate of the Slat Track No. 10 on the LH Side Sheet 01 Fig. A-UBEAA Measurement of the Aft Lug Upper Thickness of the Slat Track No. 10 on the LH Side Sheet 01 (a) At the threshold given in Tabl e 1 of the PLANNING INFORMATION paragraph E.(2): Refer to Fig. A-UFAAA Inspect the slat track No. 10 identification plate on the LH side: Refer to Fig. A-UBAAA 1 Clean the area with: Textile - Lint Free Cotton 14SBA1 As required Made moist with: Non Aqueous Cleaner - General 08BAA9 As required 2 Inspect the slat track No. 10 identification plate: Refer to Fig. A-UBAAA DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 20 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 25 @A340 SERVICE BULLETIN a If the identification plate is missing or is not readable: <1> Do SUBTASK 574148-020-401 001 Depending on the Inspection Results, Remove the Link Parts between the Slat 4 and the Slat Track No. 10 on the LH Side . And <2> Measure the aft lug upper thickness of the slat track No. 10 as shown on Fig. A-UBEAA . NOTE : Aft lug upper thickness equal to 10.80 mm (0.425 in) or 14.80 mm (0.583 in). If the dimension measured is equal to 10.80 mm (0.425 in.): [1] Do SUBTASK 574148-220-401 001 Depending on the Inspection Results, Do a Detailed Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the LH Side . And [2] Do SUBTASK 574148-250-401 001 Depending on the Inspection Results, Do an HFEC Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the LH Side . [a] If crack is found: - Upload the completed Inspection Report sheet given in Appendix 01 in accordance with ISI 00.00.00179. And - Contact AIRBUS for slat track spare preparation. And - Replace the affected slat track No. 10 by a new part number F5746412700200 at the threshold given in the Table 1 of the PLANNING INFORMATION paragraph E.(2), in accordance with TASK 574148-833-895 001 Replacement of the Slat Track(s) No. 10 . [b] If no crack is found: - Do SUBTASK 574148-420-401 001 Depending on the Inspection Results, Install the Link Parts between the Slat 4 and the Slat Track No. 10 on t h eL HS i d e. And DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 21 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 26 @A340 SERVICE BULLETIN - Identify the slat track No 10 in accordance with SUBTASK 574148-831-401 001 Depending on the Inspection Results, Identify the Slat Track No. 10 on the LH Side . And - Upload the completed Inspection Report sheet given in Appendix 01 in accordance with ISI 00.00.00179. And - Contact AIRBUS for slat track spare preparation. And - Replace the affected slat track No. 10 by a new part number F5746412700200 at the threshold given in the Table 1 of the PLANNING INFORMATION paragraph E.(2), in accordance with TASK 574148-833-895 001 Replacement of the Slat Track(s) No. 10 . If the dimension measured is not equal to 10.80 mm (0.425 in.): [1] Do SUBTASK 574148-420-401 001 Depending on the Inspection Results, Install the Link Parts between the Slat 4 and the Slat Track No. 10 on the LH Side . And [2] Do SUBTASK 574148-831-401 001 Depending on the Inspection Results, Identify the Slat Track No. 10 on the LH Side . And [3] No further action. b If the identification plate is not missing and is readable: <1> Inspect the slat track No. 10 part number. If aircraft is equipped with part number F5746411000000 or F5746411000200: [1] Do SUBTASK 574148-020-401 001 Depending on the Inspection Results, Remove the Link Parts between the Slat 4 and the Slat Track No. 10 on the LH Side . And DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 22 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 27 @A340 SERVICE BULLETIN [2] Do SUBTASK 574148-220-401 001 Depending on the Inspection Results, Do a Detailed Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the LH Side . And [3] Do SUBTASK 574148-250-401 001 Depending on the Inspection Results, Do an HFEC Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the LH Side . [a] If crack is found: - Upload the completed Inspection Report sheet given in Appendix 01 in accordance with ISI 00.00.00179. And - Contact AIRBUS for slat track spare preparation. And - Replace the affected slat track No. 10 by a new part number F5746412700200 at the threshold given in the Table 1 of the PLANNING INFORMATION paragraph E.(2), in accordance with TASK 574148-833-895 001 Replacement of the Slat Track(s) No. 10 . [b] If no crack is found: - Do SUBTASK 574148-420-401 001 Depending on the Inspection Results, Install the Link Parts between the Slat 4 and the Slat Track No. 10 on t h eL HS i d e. And - Upload the completed Inspection Report sheet given in Appendix 01 in accordance with ISI 00.00.00179. And - Contact AIRBUS for slat track spare preparation. And - Replace the affected slat track No. 10 by a new part number F5746412700200 at the threshold given in the Table 1 of the PLANNING INFORMATION paragraph E.(2), in accordance with TASK 574148-833-895 001 Replacement of the Slat Track(s) No. 10 . DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 23 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 28 @A340 SERVICE BULLETIN If aircraft is not equipped with part number F5746411000000 or F5746411000200: [1] No further action. (2) Subtask 574148-210-402-001 - Inspect the Slat Track No. 10 Identification Plate on the RH Side Work Zones and Access Panels Zone Access/Work location 622 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills NON SPECIFIC Material necessary to do the job Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner - General 08BAA9 As required Textile - Lint Free Cotton 14SBA1 As required References Fig. A-UBBAA Inspection of the Identification Plate of the Slat Track No. 10 on the RH Side Sheet 01 Fig. A-UFAAA Flowchart Sheet 01 Sheet 02 Sheet 03 Fig. A-UBFAA Measurement of the Aft Lug Upper Thickness of the Slat Track No. 10 on the RH Side Sheet 01 (a) At the threshold given in Tabl e 2 of the PLANNING INFORMATION paragraph E.(2): Refer to Fig. A-UFAAA Inspect the slat track No. 10 identification plate on the RH side: Refer to Fig. A-UBBAA DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 24 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 29 @A340 SERVICE BULLETIN 1 Clean the area with: Textile - Lint Free Cotton 14SBA1 As required Made moist with: Non Aqueous Cleaner - General 08BAA9 As required 2 Inspect the slat track No. 10 identification plate. Refer to Fig. A-UBBAA a If the identification plate is missing or is not readable: <1> Do SUBTASK 574148-020-402 001 Depending on the Inspection Results, Remove the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side . And <2> Measure the aft lug upper thickness of the slat track No. 10 as shown on Fig. A-UBFAA . NOTE : Aft lug upper thickness equal to 10.80 mm (0.425 in) or 14.80 mm (0.583 in). If the dimension measured is equal to 10.80 mm (0.425 in.): [1] Do SUBTASK 574148-220-402 001 Depending on the Inspection Results, Do a Detailed Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the RH Side . And [2] Do SUBTASK 574148-250-402 001 Depending on the Inspection Results, Do an HFEC Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the RH Side . [a] If crack is found: - Upload the completed Inspection Report sheet given in Appendix 01 in accordance with ISI 00.00.00179. And - Contact AIRBUS for slat track spare preparation. And DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 25 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 30 @A340 SERVICE BULLETIN - Replace the affected slat track No. 10 by a new part number F5746412700200 at the threshold given in the Table 2 of the PLANNING INFORMATION paragraph E.(2), in accordance with TASK 574148-833-895 001 Replacement of the Slat Track(s) No. 10 . [b] If no crack is found: - Do SUBTASK 574148-420-402 001 Depending on the Inspection Results, Install the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side . And - Identify the slat track in accordance with SUBTASK 574148-831-402 001 Depending on the Inspection Results, Identify the Slat Track No. 10 on the RH Side . And - Upload the completed Inspection Report sheet given in Appendix 01 in accordance with ISI 00.00.00179. And - Contact AIRBUS for slat track spare preparation. And - Replace the affected slat track No. 10 by a new part number F5746412700200 at the threshold given in the Table 2 of the PLANNING INFORMATION paragraph E.(2), in accordance with TASK 574148-833-895 001 Replacement of the Slat Track(s) No. 10 . If the dimension measured is not equal to 10.80 mm (0.425 in.): [1] Do SUBTASK 574148-420-402 001 Depending on the Inspection Results, Install the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side . And [2] Do SUBTASK 574148-831-402 001 Depending on the Inspection Results, Identify the Slat Track No. 10 on the RH Side . And [3] No further action. DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 26 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 31 @A340 SERVICE BULLETIN b If the identification plate is not missing and is readable: <1> Inspect the slat track No. 10 part number. If aircraft is equipped with part number F5746411000000 or F5746411000200: [1] Do SUBTASK 574148-020-402 001 Depending on the Inspection Results, Remove the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side . And [2] Do SUBTASK 574148-220-402 001 Depending on the Inspection Results, Do a Detailed Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the RH Side . And [3] Do SUBTASK 574148-250-402 001 Depending on the Inspection Results, Do an HFEC Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the RH Side . [a] If crack is found: - Upload the completed Inspection Report sheet given in Appendix 01 in accordance with ISI 00.00.00179. And - Contact AIRBUS for slat track spare preparation. And - Replace the affected slat track No. 10 by a new part number F5746412700200 at the threshold given in the Table 2 of the PLANNING INFORMATION paragraph E.(2), in accordance with TASK 574148-833-895 001 Replacement of the Slat Track(s) No. 10 . [b] If no crack is found: - Do SUBTASK 574148-420-402 001 Depending on the Inspection Results, Install the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side . And - Upload the completed Inspection Report sheet given in Appendix 01 in accordance with ISI 00.00.00179. And DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 27 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 32 @A340 SERVICE BULLETIN - Contact AIRBUS for slat track spare preparation. And - Replace the affected slat track No. 10 by a new part number F5746412700200 at the threshold given in the Table 2 of the PLANNING INFORMATION paragraph E.(2), in accordance with TASK 574148-833-895 001 Replacement of the Slat Track(s) No. 10 . If aircraft is not equipped with part number F5746411000000 or F5746411000200: [1] No further action. (3) Subtask 574148-020-401-001 - Depending on the Inspection Results, Remove the Link Parts between the Slat 4 and the Slat Track No. 10 on the LH Side Work Zones and Access Panels Zone Access/Work location 522 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Structural Repair Manual (SRM) 51-42-00 Fig. A-UBCAA Removal/Installation of the Link Parts between the Slat 4 and the Slat Track No. 10 on the LH Side Sheet 01 (a) Remove the link parts between the slat 4 and the slat track No. 10: Refer to Fig. A-UBCAA In accordance with SRM 51-42-00 1 Bolt Item (1) Retain 1 Bolt Item (2) Retain 1 Bolt Item (4) Retain 1 Bush Item (3) Retain 1 Locking Plate Item (5) Retain DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 28 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 33 @A340 SERVICE BULLETIN 1 Link Outboard Item (6) Retain 1 Link Inboard Item (8) Retain 2 Washer Item (9) Retain 1 Nut Item (7) Retain 1 Nut Item (11) Discard 1 Nut Item (12) Discard 1 Bearing Item (13) Discard 2 Pin-Cotter Item (16) Discard (4) Subtask 574148-020-402-001 - Depending on the Inspection Results, Remove the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side Work Zones and Access Panels Zone Access/Work location 622 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME References Structural Repair Manual (SRM) 51-42-00 Fig. A-UBDAA Removal/Installation of the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side Sheet 01 (a) Remove the link parts between the slat 4 and the slat track No. 10: Refer to Fig. A-UBDAA In accordance with SRM 51-42-00 1 Bolt Item (1) Retain 1 Bolt Item (2) Retain 1 Bolt Item (4) Retain 1 Bush Item (3) Retain DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 29 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 34 @A340 SERVICE BULLETIN 1 Locking Plate Item (5) Retain 1 Link Outboard Item (6) Retain 1 Link Inboard Item (8) Retain 2 Washer Item (9) Retain 1 Nut Item (7) Retain 1 Nut Item (11) Discard 1 Nut Item (12) Discard 1 Bearing Item (13) Discard 2 Pin-Cotter Item (16) Discard (5) Subtask 574148-220-401-001 - Depending on the Inspection Results, Do a Detailed Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the LH Side Work Zones and Access Panels Zone Access/Work location 522 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner - General 08BAA9 As required Textile - Lint Free Cotton 14SBA1 As required References Non Destructive Test Manual (NTM) 51-90-00 Fig. A-UBGAA Inspection of the Slat Track No. 10 on the LH Side Sheet 01 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 30 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 35 @A340 SERVICE BULLETIN References Fig. A-UFAAA Flowchart Sheet 01 Sheet 02 Sheet 03 (a) At the threshold given in Tabl e 1 of the PLANNING INFORMATION paragraph E.(2): Refer to Fig. A-UFAAA Do a detailed inspection in the upper area of the aft lug of the slat track No. 10 on the LH side: Refer to Fig. A-UBGAA 1 Use a non metallic spatula to remove the sealant and clean the area with: Textile - Lint Free Cotton 14SBA1 As required Made moist with: Non Aqueous Cleaner - General 08BAA9 As required 2 Do a detailed visual inspection, refer to NTM 51-90-00. (6) Subtask 574148-220-402-001 - Depending on the Inspection Results, Do a Detailed Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the RH Side Work Zones and Access Panels Zone Access/Work location 622 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner - General 08BAA9 As required Textile - Lint Free Cotton 14SBA1 As required DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 31 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 36 @A340 SERVICE BULLETIN References Non Destructive Test Manual (NTM) 51-90-00 Fig. A-UBHAA Inspection of the Slat Track No. 10 on the RH Side Sheet 01 Fig. A-UFAAA Flowchart Sheet 01 Sheet 02 Sheet 03 (a) At the threshold given in Tabl e 2 of the PLANNING INFORMATION paragraph E.(2): Refer to Fig. A-UFAAA Do a detailed inspection in the upper area of the aft lug of the slat track No. 10 on the RH side: Refer to Fig. A-UBHAA 1 Use a non metallic spatula to remove the sealant and clean the area with: Textile - Lint Free Cotton 14SBA1 As required Made moist with: Non Aqueous Cleaner - General 08BAA9 As required 2 Do a detailed visual inspection, refer to NTM 51-90-00. (7) Subtask 574148-250-401-001 - Depending on the Inspection Results, Do an HFEC Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the LH Side Work Zones and Access Panels Zone Access/Work location 522 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills NON DESTRUCTIVE TESTING DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 32 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 37 @A340 SERVICE BULLETIN Material necessary to do the job Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner - General 08BAA9 As required Textile - Lint Free Cotton 14SBA1 As required References Non Destructive Test Manual (NTM) 51-10-08 Fig. A-UBGAA Inspection of the Slat Track No. 10 on the LH Side Sheet 01 Fig. A-UFAAA Flowchart Sheet 01 Sheet 02 Sheet 03 (a) At the threshold given in Tabl e 1 of the PLANNING INFORMATION paragraph E.(2): Refer to Fig. A-UFAAA Do a High Frequency Eddy Current (HFEC) inspection in the upper area of the aft lug of the slat track No. 10 on the LH side: Refer to Fig. A-UBGAA 1 Use a non metallic spatula to remove the sealant and clean the area with: Textile - Lint Free Cotton 14SBA1 As required Made moist with: Non Aqueous Cleaner - General 08BAA9 As required 2 Do an HFEC inspection in the upper area of the aft lug of the slat track No. 10 on the LH side, refer to NTM 51-10-08. (8) Subtask 574148-250-402-001 - Depending on the Inspection Results, Do an HFEC Inspection in the Upper Area of the Aft Lug of the Slat Track No. 10 on the RH Side Work Zones and Access Panels Zone Access/Work location 622 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 33 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 38 @A340 SERVICE BULLETIN Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills NON DESTRUCTIVE TESTING Material necessary to do the job Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner - General 08BAA9 As required Textile - Lint Free Cotton 14SBA1 As required References Non Destructive Test Manual (NTM) 51-10-08 Fig. A-UBHAA Inspection of the Slat Track No. 10 on the RH Side Sheet 01 Fig. A-UFAAA Flowchart Sheet 01 Sheet 02 Sheet 03 (a) At the threshold given in Tabl e 2 of the PLANNING INFORMATION paragraph E.(2): Refer to Fig. A-UFAAA Do an HFEC inspection in the upper area of the aft lug of the slat track No. 10 on the RH side: Refer to Fig. A-UBHAA 1 Use a non metallic spatula to remove the sealant and clean the area with: Textile - Lint Free Cotton 14SBA1 As required Made moist with: Non Aqueous Cleaner - General 08BAA9 As required 2 Do an HFEC inspection in the upper area of the aft lug of the slat track No. 10 on the RH side, refer to NTM 51-10-08. DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 34 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 39 @A340 SERVICE BULLETIN (9) Subtask 574148-420-401-001 - Depending on the Inspection Results, Install the Link Parts between the Slat 4 and the Slat Track No. 10 on the LH Side Work Zones and Access Panels Zone Access/Work location 522 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPB01 ITEM NEW PART N˚ QTY (UM) KEYWORD SEE NOTES 11 NSA5059C12 1 NUT 12 NSA5059C10 1 NUT 13 ABS0571-14W 1 BEARING 16 MS24665-376 2 PIN NOTE : The components listed above are only necessary if the identification plate is missing or is not readable, and no crack is found. The quantity of these items are to be ordered as required. NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Mineral Base Lubricating Oil - General and Water-Disp 03BDB9 As required Synthetic Oil Base Grease - General Purpose Clay Th 03GBB1 As required Coating - Flexible Structure 04QAB2 As required Polysulfide Sealant - General Purpose Brushable 06AAA1 As required Polysulfide Sealant - General Purpose Fillet 06AAB1 As required Polysulfide Sealant - Fuel Tank Brushable 06ABA1 As required References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-801 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 35 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 40 @A340 SERVICE BULLETIN References Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-75-12 Fig. A-UBCAA Removal/Installation of the Link Parts between the Slat 4 and the Slat Track No. 10 on the LH Side Sheet 01 (a) Install the link parts between the slat 4 and the slat track No. 10: 1 Protect temporarily the unpainted areas of the track with: Refer to Fig. A-UBCAA Mineral Base Lubricating Oil - General and Water- Disp 03BDB9 As required 2 Install the bearing: Refer to Fig. A-UBCAA 1 Bearing ABS0571-14W Item 13 Apply interfay sealant with: In accordance with SRM 51-24-00 Polysulfide Sealant - General Purpose Brushable 06AAA1 As required Apply external fillet sealing with: In accordance with SRM 51-24-00 Polysulfide Sealant - General Purpose Fillet 06AAB1 As required 3 Install the link parts: In accordance with SRM 51-40-00, SRM 51-42-00 and SRM 51-43-00 Refer to AMM Task 20-21-11-911-801 Refer to Fig. A-UBCAA 1 Bolt Item (1) Retained at removal DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 36 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 41 @A340 SERVICE BULLETIN 1 Bolt Item (2) Retained at removal 1 Bolt Item (4) Retained at removal 1 Bush Item (3) Retained at removal 1 Locking Plate Item (5) Retained at removal 1 Link Outboard Item (6) Retained at removal 1 Link Inboard Item (8) Retained at removal 2 Washer Item (9) Retained at removal 1 Nut Item (7) Retained at removal 1 Nut NSA5059C12 Item 11 Tigthen the nut to a torque value comprised between 4.60 m.daN and 7.60 m.daN (407.135 lbf.in. and 672.656 lbf.in.). 1 Nut NSA5059C10 Item 12 Tigthen the nut to a torque value comprised between 3.40 m.daN and 4.80 m.daN (300.926 lbf.in. and 424.835 lbf.in.). 2 Pin-Cotter MS24665-376 Item 16 Lubricate the pins with: Synthetic Oil Base Grease - General Purpose Clay Th 03GBB1 As required Overcoat the bolts and nuts with: In accordance with SRM 51-24-00 Polysulfide Sealant - Fuel Tank Brushable 06ABA1 As required Protect the fastener heads with: In accordance with SRM 51-75-12 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 37 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 42 @A340 SERVICE BULLETIN Coating - Flexible Structure 04QAB2 As required (10) Subtask 574148-420-402-001 - Depending on the Inspection Results, Install the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side Work Zones and Access Panels Zone Access/Work location 622 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPB01 ITEM NEW PART N˚ QTY (UM) KEYWORD SEE NOTES 11 NSA5059C12 1 NUT 12 NSA5059C10 1 NUT 13 ABS0571-14W 1 BEARING 16 MS24665-376 2 PIN NOTE : The components listed above are only necessary if the identification plate is missing or is not readable, and no crack is found. The quantity of these items are to be ordered as required. NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Mineral Base Lubricating Oil - General and Water-Disp 03BDB9 As required Synthetic Oil Base Grease - General Purpose Clay Th 03GBB1 As required Coating - Flexible Structure 04QAB2 As required Polysulfide Sealant - General Purpose Brushable 06AAA1 As required Polysulfide Sealant - General Purpose Fillet 06AAB1 As required Polysulfide Sealant - Fuel Tank Brushable 06ABA1 As required DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 38 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 43 @A340 SERVICE BULLETIN References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-801 Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-75-12 Fig. A-UBDAA Removal/Installation of the Link Parts between the Slat 4 and the Slat Track No. 10 on the RH Side Sheet 01 (a) Install the link parts between the slat 4 and the slat track No. 10: 1 Protect temporarily the unpainted areas of the track with: Refer to Fig. A-UBDAA Mineral Base Lubricating Oil - General and Water- Disp 03BDB9 As required 2 Install the bearing: Refer to Fig. A-UBDAA 1 Bearing ABS0571-14W Item 13 Apply interfay sealant with: In accordance with SRM 51-24-00 Polysulfide Sealant - General Purpose Brushable 06AAA1 As required Apply external fillet sealing with: In accordance with SRM 51-24-00 Polysulfide Sealant - General Purpose Fillet 06AAB1 As required 3 Install the link parts: In accordance with SRM 51-40-00, SRM 51-42-00 and SRM 51-43-00 Refer to AMM Task 20-21-11-911-801 Refer to Fig. A-UBDAA DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 39 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 44 @A340 SERVICE BULLETIN 1 Bolt Item (1) Retained at removal 1 Bolt Item (2) Retained at removal 1 Bolt Item (4) Retained at removal 1 Bush Item (3) Retained at removal 1 Locking Plate Item (5) Retained at removal 1 Link Outboard Item (6) Retained at removal 1 Link Inboard Item (8) Retained at removal 2 Washer Item (9) Retained at removal 1 Nut Item (7) Retained at removal 1 Nut NSA5059C12 Item 11 Tigthen the nut to a torque value comprised between 4.60 m.daN and 7.60 m.daN (407.135 lbf.in. and 672.656 lbf.in.). 1 Nut NSA5059C10 Item 12 Tigthen the nut to a torque value comprised between 3.40 m.daN and 4.80 m.daN (300.926 lbf.in. and 424.835 lbf.in.). 2 Pin-Cotter MS24665-376 Item 16 Lubricate the pins with: Synthetic Oil Base Grease - General Purpose Clay Th 03GBB1 As required Overcoat the bolts and nuts with: In accordance with SRM 51-24-00 Polysulfide Sealant - Fuel Tank Brushable 06ABA1 As required DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 40 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 45 @A340 SERVICE BULLETIN Protect the fastener heads with: In accordance with SRM 51-75-12 Coating - Flexible Structure 04QAB2 As required (11) Subtask 574148-831-401-001 - Depending on th e Inspection Results, Identify the Slat Track No. 10 on the LH Side Work Zones and Access Panels Zone Access/Work location 522 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPB01 ITEM NEW PART N˚ QTY (UM) KEYWORD SEE NOTES 18 NSA9117-22B 1 PLATE NOTE : The components listed above are only necessary if the identification plate is missing or is not readable, and no crack is found. The quantity of these items are to be ordered as required. NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner - General 08BAA9 As required Paste Adhesive-Epoxy Potting Structure 13FBB2 As required Textile - Lint Free Cotton 14SBA1 As required References Process and Material Specification (PMS) Process and Material Specification (PMS) 01-06-13 Structural Repair Manual (SRM) 51-24-00 Fig. A-UBMAA Identification of the Slat Track No. 10 on the LH Side Sheet 01 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 41 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 46 @A340 SERVICE BULLETIN (a) Identify the slat track No. 10: Refer to Fig. A-UBMAA 1 Remove the identification plate: 1 Identification Plate Item (18) Discard NOTE : If the identification plate is missing, go to the next step. 2 Identify the part number: Refer to Process and Material Specification (PMS) 01-06-13 NOTE : The plate identification and exchange is described in OIT No. 999-0058/16, OIT No. 999-0066/17, ISI No. 00.00.00285, ISI No. 00.05.00003 and ISI No. 11.00.00002. a In case of the slat track No. 10 reference number can be identified via documentation or because no exchange of part since delivery, write the corresponding part number on the identification plate, item 18. b In case of difficulties to identify the part number of the slat track No. 10, contact AIRBUS. 3 Use a non metallic spatula to remove the sealant and clean the area with: Textile - Lint Free Cotton 14SBA1 As required Made moist with: Non Aqueous Cleaner - General 08BAA9 As required 4 Install the identification plate: 1 Identification Plate NSA9117-22B Item 18 Install with: In accordance with SRM 51-24-00 Paste Adhesive- Epoxy Potting Structure 13FBB2 As required (12) Subtask 574148-831-402-001 - Depending on th e Inspection Results, Identify the Slat Track No. 10 on the RH Side Work Zones and Access Panels Zone Access/Work location 622 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 42 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 47 @A340 SERVICE BULLETIN Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPB01 ITEM NEW PART N˚ QTY (UM) KEYWORD SEE NOTES 18 NSA9117-22B 1 PLATE NOTE : The components listed above are only necessary if the identification plate is missing or is not readable, and no crack is found. The quantity of these items are to be ordered as required. NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Non Aqueous Cleaner - General 08BAA9 As required Paste Adhesive-Epoxy Potting Structure 13FBB2 As required Textile - Lint Free Cotton 14SBA1 As required References Process and Material Specification (PMS) Process and Material Specification (PMS) 01-06-13 Structural Repair Manual (SRM) 51-24-00 Fig. A-UBLAA Identification of the Slat Track No. 10 on the RH Side Sheet 01 (a) Identify the slat track No. 10: Refer to Fig. A-UBLAA 1 Remove the identification plate: 1 Identification Plate Item (18) Discard NOTE : If the identification plate is missing, go to the next step. 2 Identify the part number: Refer to Process and Material Specification (PMS) 01-06-13 DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 43 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 48 @A340 SERVICE BULLETIN NOTE : The plate identification and exchange is described in OIT No. 999-0058/16, OIT No. 999-0066/17, ISI No. 00.00.00285, ISI No. 00.05.00003 and ISI No. 11.00.00002. a In case of the slat track No. 10 reference number can be identified via documentation or because no exchange of part since delivery, write the corresponding part number on the identification plate, item 18. b In case of difficulties to identify the part number of the slat track No. 10, contact AIRBUS. 3 Use a non metallic spatula to remove the sealant and clean the area with: Textile - Lint Free Cotton 14SBA1 As required Made moist with: Non Aqueous Cleaner - General 08BAA9 As required 4 Install the identification plate: 1 Identification Plate NSA9117-22B Item 18 Install with: In accordance with SRM 51-24-00 Paste Adhesive- Epoxy Potting Structure 13FBB2 As required D. TEST None E. CLOSE-UP NOTE : If you intend to accomplish an associated Repair Task during the same layover period, the subsequent Close-up procedure is not necessary. (1) Subtask 574148-942-401-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 27-80-00-866-802 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Remove the access platform(s). DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 44 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 49 @A340 SERVICE BULLETIN (c) Retract the slats, refer to AMM Task 27-80-00-866-802. (d) Put the aircraft back to its initial configuration. DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 45 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 50 @A340 SERVICE BULLETIN This Page Intentionally Left Blank DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 46 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 51 @A340 SERVICE BULLETIN Task 574148-833-895-001 - Replacement of the Slat Track(s) No. 10 WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE) . WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: - PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC., AS NECESSARY ON WIRING AND COMPONENTS. - REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00. NOTE : The accomplishment instructions of this Service Bulletin include procedures given in other documents or in other sections of the Service Bulletin. When the words ’refer to’ are used and the operator has a procedure accepted by the local authority he belongs to, the accepted alternative procedure can be used. When the words ’in accordance with’ are used then the given procedure must be followed. NOTE : The access and close-up instructions, not comprising return to service tests, in this Service Bulletin do not constitute or affect the technical intent of the Service Bulletin. Operators can therefore, as deemed necessary, omit or add access and/or close-up steps to add flexibility to their maintenance operations as long as the technical intent of the Service Bulletin is met within the set parameters. NOTE : Manual titles given in the accomplishment instructions are referred to by acronyms. Refer to paragraph 1.J., References, for the definition of acronyms. NOTE : This Service Bulletin contains the instructions for the on-aircraft maintenance necessary to ensure the continued airworthiness of the aircraft. For any deviations to the instructions, including RC paragraph contained herein, contact AIRBUS for further instructions and approval. NOTE : This Service Bulletin is classified mandatory or expected to be classified mandatory by an Airworthiness Directive (AD). The paragraphs 3.C. and 3.D. in these accomplishment instructions are Required for Compliance (RC) and must be done to comply with the AD. To allow more flexibility, the rule "refer to" and "in accordance with" will apply to these paragraphs 3.C. and 3.D. Other paragraphs are recommended and may be deviated from, done as part of other actions or done with accepted methods different from those given in the Service Bulletin, as long as the RC paragraphs can be done and the aircraft can be put back into a serviceable condition. DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 47 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 52 @A340 SERVICE BULLETIN NOTE : Discarded parts must be managed at the operator’s discretion. Task Associated Data Zone 522 622 Manpower TOTAL MANHOURS 8.00 ELAPSED TIME (HOURS) 4.00 A. GENERAL (1) Subtask 574148-910-402-001 - Standard Practices Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-20-00, Page Block 001 Task 20-21-11-911-801 Consumable Material List (CML) Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-75-12 (a) For the identification of zones, refer to AMM 06-20-00, Page Block 001. (b) If alternative and substitute fasteners have to be used, you must make sure that the associated nut/collar are compatible in accordance with SRM 51-40-00 ’Mating Part’ column. (c) Remove and install fasteners in accordance with SRM 51-42-00. (d) Get alternative and substitute fastener data in accordance with SRM 51-43-00. (e) To torque tighten the standard threaded fasteners, refer to AMM Task 20-21-11-911-801. (f) Apply sealant in accordance with SRM 51-24-00. (g) For the specification of Material Numbers (Mat. No.) given in this Service Bulletin, refer to the Consumable Materials List (CML). (h) Renew the protective finish in accordance with SRM 51-75-12. (i) Tag all the parts you must remove and retain to make the subsequent installation easier. (j) Put all the retained hardware in identified plastic bags and attach the bags to the related unit. DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 48 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 53 @A340 SERVICE BULLETIN (2) Subtask 574148-839-402-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. B. PREPARATION NOTE : If you intend to accomplish this Repair Task during the same layover period as the associated Inspection, the subsequent General Job Set-up procedure is not necessary. (1) Subtask 574148-941-402-001 - General Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 12-34-24-860-802 NOTE : For the basic Aircraft configuration, refer to AMM Chapter "Introduction - Aircraft status for maintenance" in Manual Front Matter section. (a) Make sure that the aircraft is electrically grounded, refer to AMM Task 12-34-24-860-802. (2) Subtask 574148-941-403-001 - Job Set-up on the LH Side Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 27-84-69-000-801 (a) Do the job set-up as specify in the removal of the slat tracks No. 5 thru 16, refer to AMM Task 27-84-69-000-801. (3) Subtask 574148-941-404-001 - Job Set-up on the RH Side Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) Task 27-84-69-000-801 (a) Do the job set-up as specify in the removal of the slat tracks No. 5 thru 16, refer to AMM Task 27-84-69-000-801. DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 49 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 54 @A340 SERVICE BULLETIN C. PROCEDURE (1) Subtask 574148-960-401-001 - Depending on the Inspection Results, Replace the Slat Track No. 10 on the LH Side Work Zones and Access Panels Zone Access/Work location 522 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Component COMPB02 ITEM NEW PART N˚ QTY (UM) KEYWORD SEE NOTES 11 NSA5059C12 1 NUT 12 NSA5059C10 2 NUT 16 MS24665-376 3 PIN NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE : The components listed above are only necessary if the slat track No. 10 is replaced. The quantity of these items are to be ordered as required. Component COMPB03 ITEM NEW PART N˚ QTY (UM) KEYWORD SEE NOTES 19 F5746412700200 1 TRACK NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE : The components listed above are only necessary if the slat track No. 10 is replaced. The quantity of these items are to be ordered as required. Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Mineral Base Lubricating Oil - General and Water-Disp 03BDB9 As required Synthetic Oil Base Grease - General Purpose Clay Th 03GBB1 As required Coating - Flexible Structure 04QAB2 As required DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 50 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 55 @A340 SERVICE BULLETIN ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Polysulfide Sealant - Fuel Tank Brushable 06ABA1 As required References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-801 Task 27-84-69-000-801 Task 27-84-69-400-801 Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-75-12 Fig. A-UBIAA Replacement of the Slat Track No. 10 on the LH Side Sheet 01 (a) Replace the slat track No. 10 on the LH side: 1 Remove the link parts between the slat 4 and the slat track No. 10: Refer to Fig. A-UBIAA In accordance with SRM 51-42-00 1 Bolt Item (1) Retain 1 Bolt Item (2) Retain 1 Bolt Item (4) Retain 1 Bolt Item (10) Retain 1 Bush Item (3) Retain 1 Locking Plate Item (5) Retain 1 Link Outboard Item (6) Retain 1 Link Inboard Item (8) Retain 1 Link Plate Outboard Item (14) Retain 1 Link Plate Inboard Item (15) Retain 3 Pin-Cotter Item (16) Discard 2 Washer Item (9) Retain DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 51 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 56 @A340 SERVICE BULLETIN 1 Washer Item (17) Retain 1 Nut Item (7) Retain 2 Nut Item (12) Discard 1 Nut Item (11) Discard NOTE : If you intend to accomplish this Repair Task during the same layover period as the associated Inspection, some items are already removed. 2 Remove the slat track No. 10, refer to AMM Task 27-84-69-000-801: Refer to Fig. A-UBIAA 1 Track Assy-No 10 Item (19) Discard 3 Install the new slat track No. 10, refer to AMM Task 27-84-69-400-801: Refer to Fig. A-UBIAA 1 Track Assy-No 10 F5746412700200 Item 19 4 Install the link parts between the slat 4 and the slat track No. 10: a Protect temporarily the unpainted areas of the track with: Refer to Fig. A-UBIAA Mineral Base Lubricating Oil - General and Water- Disp 03BDB9 As required b Install the link plates: In accordance with SRM 51-40-00, SRM 51-42-00 and SRM 51-43-00 Refer to AMM Task 20-21-11-911-801 Refer to Fig. A-UBIAA 1 Link Plate Outboard Item (14) Retained at removal 1 Link Plate Inboard Item (15) Retained at removal 1 Bolt Item (1) Retained at removal DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 52 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 57 @A340 SERVICE BULLETIN 1 Bolt Item (10) Retained at removal 1 Washer Item (9) Retained at removal 1 Washer Item (17) Retained at removal 1 Nut NSA5059C12 Item 11 Tigthen the nut to a torque value comprised between 4.60 m.daN and 7.60 m.daN (407.135 lbf.in. and 672.656 lbf.in.). 1 Nut NSA5059C10 Item 12 Tigthen the nut to a torque value comprised between 3.40 m.daN and 4.80 m.daN (300.926 lbf.in. and 424.835 lbf.in.). 2 Pin-Cotter MS24665-376 Item 16 Lubricate the pins with: Synthetic Oil Base Grease - General Purpose Clay Th 03GBB1 As required Overcoat the bolts and nuts with: In accordance with SRM 51-24-00 Polysulfide Sealant - Fuel Tank Brushable 06ABA1 As required Protect the fastener heads with: In accordance with SRM 51-75-12 Coating - Flexible Structure 04QAB2 As required c Install the link parts: In accordance with SRM 51-40-00, SRM 51-42-00 and SRM 51-43-00 Refer to AMM Task 20-21-11-911-801 Refer to Fig. A-UBIAA 1 Bolt Item (2) Retained at removal DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 53 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 58 @A340 SERVICE BULLETIN 1 Bolt Item (4) Retained at removal 1 Bush Item (3) Retained at removal 1 Locking Plate Item (5) Retained at removal 1 Link Outboard Item (6) Retained at removal 1 Link Inboard Item (8) Retained at removal 1 Washer Item (9) Retained at removal 1 Nut Item (7) Retained at removal 1 Nut NSA5059C10 Item 12 Tigthen the nut to a torque value comprised between 3.40 m.daN and 4.80 m.daN (300.926 lbf.in. and 424.835 lbf.in.). 1 Pin-Cotter MS24665-376 Item 16 Lubricate the pins with: Synthetic Oil Base Grease - General Purpose Clay Th 03GBB1 As required Overcoat the bolts and nuts with: In accordance with SRM 51-24-00 Polysulfide Sealant - Fuel Tank Brushable 06ABA1 As required Protect the fastener heads with: In accordance with SRM 51-75-12 Coating - Flexible Structure 04QAB2 As required DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 54 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 59 @A340 SERVICE BULLETIN (2) Subtask 574148-960-402-001 - Depending on the Inspection Results, Replace the Slat Track No. 10 on the RH Side Work Zones and Access Panels Zone Access/Work location 622 Manpower Resources Manhours 3.00 Minimum number of person 1 Subtask elapsed time 3.00 Skills AIRFRAME Material necessary to do the job Component COMPB02 ITEM NEW PART N˚ QTY (UM) KEYWORD SEE NOTES 11 NSA5059C12 1 NUT 12 NSA5059C10 2 NUT 16 MS24665-376 3 PIN NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE : The components listed above are only necessary if the slat track No. 10 is replaced. The quantity of these items are to be ordered as required. Component COMPB03 ITEM NEW PART N˚ QTY (UM) KEYWORD SEE NOTES 19 F5746412700200 1 TRACK NOTE : The above list of components is not an AIRBUS Kit, the required parts shall be ordered as necessary through the given channel. NOTE : The components listed above are only necessary if the slat track No. 10 is replaced. The quantity of these items are to be ordered as required. Consumable CMLB01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Mineral Base Lubricating Oil - General and Water-Disp 03BDB9 As required Synthetic Oil Base Grease - General Purpose Clay Th 03GBB1 As required Coating - Flexible Structure 04QAB2 As required Polysulfide Sealant - Fuel Tank Brushable 06ABA1 As required DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 55 7 Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved. ### Page 60 @A340 SERVICE BULLETIN References Aircraft Maintenance Manual (AMM) Task 20-21-11-911-801 Task 27-84-69-000-801 Task 27-84-69-400-801 Structural Repair Manual (SRM) 51-24-00 51-40-00 51-42-00 51-43-00 51-75-12 Fig. A-UBJAA Replacement of the Slat Track No. 10 on the RH Side Sheet 01 (a) Replace the slat track No. 10 on the RH side: 1 Remove the link parts between the slat 4 and the slat track No. 10: Refer to Fig. A-UBJAA In accordance with SRM 51-42-00 1 Bolt Item (1) Retain 1 Bolt Item (2) Retain 1 Bolt Item (4) Retain 1 Bolt Item (10) Retain 1 Bush Item (3) Retain 1 Locking Plate Item (5) Retain 1 Link Outboard Item (6) Retain 1 Link Inboard Item (8) Retain 1 Link Plate Outboard Item (14) Retain 1 Link Plate Inboard Item (15) Retain 3 Pin-Cotter Item (16) Discard 2 Washer Item (9) Retain 1 Washer Item (17) Retain 1 Nut Item (7) Retain DATE: Nov 12/18 SERVICE BULLETIN No.: A340-57-4148 REVISION No.: 00 - Nov 12/18 Page: 56 7 Printed in FRANCE © AIRBUS S.A.S. 2007. 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