# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 53 

### TITLE: FUSELAGE - CENTER FUSELAGE - INSPECTION OF RODS IN BELLY FAIRING MODIFICATION No.: None This page transmits Revision No.01 of Service Bulletin No.A340-53-4185 ADDITIONAL WORK **CONF ALL No additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 01 issued to redefine item numbers of the rods at FR39. CHANGES SUMMARY EFFECTIVITY OPERATOR LIST UPDATED R Fig. A-FSAAA Fig. A-FSAAA Sheet 01 SHEET UPDATED R PLANNING INFORMATION EFFECTIVITY EFFECTIVITY RELATED INFORMATION UPDATED R Material Effectivity MATERIAL EFFECTIVITY UPDATED MATERIAL SET QUANTITY UPDATED R ACCOMPLISHMENT INSTRUCTIONS TASK 534185- 832-801-001-Inspection Subtask 534185-020-001-001 SUBTASK SOLUTION ADDED N Subtask 534185-020-002-001 SUBTASK SOLUTION ADDED N Subtask 534185-420-001-001 SUBTASK SOLUTION ADDED N Subtask 534185-420-002-001 SUBTASK SOLUTION ADDED N TASK 534185- 832-802-001-Inspection Subtask 534185-020-003-001 SUBTASK SOLUTION ADDED N Subtask 534185-020-004-001 SUBTASK SOLUTION ADDED N
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 1 5

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# @A340 SERVICE BULLETIN REVISION TRANSMITTAL SHEET
Subtask 534185-833-001-001 SUBTASK SOLUTION UPDATED PART NUMBER UPDATED ITEM NUMBER UPDATED MATERIAL LIST UPDATED R

Subtask 534185-833-002-001 SUBTASK SOLUTION UPDATED PART NUMBER UPDATED ITEM NUMBER UPDATED MATERIAL LIST UPDATED R

Subtask 534185-420-003-001 SUBTASK SOLUTION ADDED N Subtask 534185-420-004-001 SUBTASK SOLUTION ADDED N Fig. A-FBAAA Fig. A-FBAAA Sheet 01 SHEET UPDATED R Fig. A-FBBAA Fig. A-FBBAA Sheet 01 SHEET UPDATED R Fig. A-FBCAA Fig. A-FBCAA Sheet 01 SHEET UPDATED R Fig. A-FBCAA Sheet 02 SHEET UPDATED R Fig. A-FBDAA FIGURE SOLUTION ADDED N Fig. A-FBDAA Sheet 01 SHEET ADDED N Appendix 01 Fig. A-FAAAA Fig. A-FAAAA Sheet 02 SHEET UPDATED R FILLING INSTRUCTIONS This Service Bulletin has been generated electronically and is reissued as a complete document. Replace the complete document. Put this Revision Transmittal Sheet in front of the Service Bulletin. HISTORY OF PREVIOUS REVISIONS No previous revision REVISION SEQUENCE ORIGINAL: Jan 17/11 REVISION No. : 01 - Apr 07/11

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 2 5

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# @A340 SERVICE BULLETIN SUMMARY AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51 This summary is for information only and is not approved for modification of the aircraft. 

# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 53 

### TITLE: FUSELAGE - CENTER FUSELAGE - INSPECTION OF RODS IN BELLY FAIRING **CONF ALL MODIFICATIONS None REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES A rod manufacturing process defect has been identified at TAC that could have led to deliver rods with cracks (crimped end of the rod only). This Inspection Service Bulletin (ISB) requires to inspect some rods in the belly fairing. Those rods can be manufactured by either SARMA-SKF or by TAC. - If they are manufactured by SARMA-SKF, no further action is required. - If they are manufactured by TAC, it is mandatory within 6 years from the ISB issuance to perform a Non Destructive Test (NDT) inspection at the crimped end of the rod body. Cracked TAC rods must be replaced. Accomplishment of this ISB will prevent any cracks on rods installed on the belly fairing. 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: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 1 5

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# @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 COMPA01 1 See SB Rod Component COMPA02 1 See SB Pin EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

47W 56W 83V AAW AFR AIB ALK ARG B3R CAL CCA CES CPA DGA DLH FIN GAF GFA HFY IBE KAC LAN LHT M3R MAU MSR NMB OAL PAL QAF R3L RJA S3R SAA SAS SFW SLM SVW SWR TAP THT THY UAE VCV VIR XAX CONCURRENT REQUIREMENTS None REFERENCES / REPERCUSSIONS TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT YES EQUIPMENT NO HARD NO SOFT NO OBRM NO MANPOWER Task 534185-832-801-001: Inspection TOTAL MANHOURS 7.25 ELAPSED TIME (HOURS) 7.25 Task 534185-832-802-001: Inspection TOTAL MANHOURS 13.00 ELAPSED TIME (HOURS) 13.00

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 2 5

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# @A340 SERVICE BULLETIN SUMMARY APPENDICES Appendix 01

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 3 5

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# @A340 SERVICE BULLETIN SUMMARY

**CONF ALL

FR37 FR39 FR48 FR53.2 FR53.9



### B **B B**  **B**

**B B**  **B B**  **B**



## A MANUFACTURER AND PN TO BE IDENTIFIED



## B TYPICAL 

### A Z190



### C

**C**

F_SB_534185_5_SAAA_01_02 Figure A-FSAAA - Sheet 01

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 4 5

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# @A340 SERVICE BULLETIN SUMMARY

**CONF ALL

AREA TO BE

TYPICAL CRACK INSPECTED

LOCATION

TYPICAL 

## C

F_SB_534185_5_SAAA_02_00 Figure A-FSAAA - Sheet 02

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 5 5

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# @A340 SERVICE BULLETIN SUMMARY

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# @A340 SERVICE BULLETIN
AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F Fax : (33) 5 61 93 42 51



# MANDATORY MANDATORY MANDATORY
ATA SYSTEM: 53 

### TITLE: FUSELAGE - CENTER FUSELAGE - INSPECTION OF RODS IN BELLY FAIRING 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 340-211 340-212 340-213 340-311 340-312 340-313 (2) Effectivity by MSN 0002-0006 0008-0009 0011 0013-0015 0018-0029 0031-0035 0038-0041 0043-0044 0046-0049 0051-0053 0056-0058 0061 0063 0074-0076 0078-0081 0084-0085 0088-0091 0093-0094 0097 0101 0103-0104 0114-0115 0117 0123 0125-0126 0128-0129 0131 0133-0137 0139 0141-0142 0145-0147 0149-0152 0154 0156-0161 0163-0164 0166-0170 0173-0176 0178-0180 0182 0185-0187 0190 0192-0194 0196-0197 0199 0201-0202 0204 0207-0208 0210 0212-0218 0220-0221 0225 0227-0228 0233 0235-0237 0239 0242-0243 0245-0246 0252 0257 0260 0263-0264 0268 0270 0273-0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318-0319 0321 0325 0327 0329 0331-0332 0335 0347 0352 0354-0355 0359 0363 0367 0373-0374 0377-0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413-0415 0424 0429-0430 0433-0435 0438 0442 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: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 1 5

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# @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 47W 0009 56W 0013 83V 0039 0040 0097 0103 0133 AAW 0151 AFR 0029 0078 0084 0186 0207 0210 0237 0245 0246 0260 0307 0310 0319 0373 0377 0399 AIB 0414 ALK 0032 0033 0034 0367 0374 ARG 0048 0063 0074 0080 0085 0093 0094 B3R 0046 CAL 0402 0406 0411 0415 0433 0541 CCA 0192 0199 0201 0242 0243 0264 CES 0129 0131 0141 0161 0182 CPA 0123 0126 0128 0136 0137 0142 0147 0157 0160 0208 0218 0220 0227 0228 0381 DGA 0075 0081 DLH 0020 0024 0027 0028 0035 0052 0053 0056 0135 0158 0213 0233 0252 0297 0304 0321 0325 0327 0335 0347 0352 0354 0379 0390 0434 0447 FIN 0058 0168 0174 0835 0844 0921 0938 GAF 0274 GFA 0212 0215 0282 0554 HFY 0117 0450 IBE 0005 0088 0125 0134 0145 0146 0170 0193 0217 0221 0302 0318 0329 0332 0387 0459 0474 0483 KAC 0089 0090 0101 0104 LAN 0167 0359 0363 0429 0442 LHT 0355 M3R 0061 MAU 0076 0152 0194 0268 0793 0800 MSR 0156 0159 0178 NMB 0047 0051 OAL 0235 0239 0280 0292 PAL 0173 0176 0187 0196 QAF 0026 0528 R3L 0004 RJA 0014 0022 0038 0043 S3R 0204 SAA 0006 0008 0011 0018 0019 0021 0197 0378 0544 0582 0590 0643 0646 0651
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# @A340 SERVICE BULLETIN

OPERATOR MSN SAS 0413 0424 0430 0435 0467 0470 SFW 0015 SLM 0049 SVW 0955 SWR 0150 0154 0169 0175 0179 0263 0538 0545 0546 0556 0559 0561 0562 0585 0598 TAP 0041 0044 0079 0091 THT 0385 0395 0438 0446 0668 THY 0023 0025 0057 0115 0180 0216 0257 0270 0331 UAE 0139 0149 0163 0166 0185 0190 0202 0236 VCV 0031 VIR 0002 0003 0114 0164 0214 0225 XAX 0273 0278 (4) Configuration by MSN MSN CONFIGURATION 0002 0003 0004 0005 0006 0008 0009 0011 0013 0014 0015 0018 0019 0020 0021 0022 0023 0024 0025 0026 0027 0028 0029 0031 0032 0033 0034 0035 0038 0039 0040 0041 0043 0044 0046 0047 0048 0049 0051 0052 0053 0056 0057 0058 0061 0063 0074 0075 0076 0078 0079 0080 0081 0084 0085 0088 0089 0090 0091 0093 0094 0097 0101 0103 0104 0114 0115 0117 0123 0125 0126 0128 0129 0131 0133 0134 0135 0136 0137 0139 0141 0142 0145 0146 0147 0149 0150 0151 0152 0154 0156 0157 0158 0159 0160 0161 0163 0164 0166 0167 0168 0169 0170 0173 0174 0175 0176 0178 0179 0180 0182 0185 0186 0187 0190 0192 0193 0194 0196 0197 0199 0201 0202 0204 0207 0208 0210 0212 0213 0214 0215 0216 0217 0218 0220 0221 0225 0227 0228 0233 0235 0236 0237 0239 0242 0243 0245 0246 0252 0257 0260 0263 0264 0268 0270 0273 0274 0278 0280 0282 0292 0297 0302 0304 0307 0310 0318 0319 0321 0325 0327 0329 0331 0332 0335 0347 0352 0354 0355 0359 0363 0367 0373 0374 0377 0378 0379 0381 0385 0387 0390 0395 0399 0402 0406 0411 0413 0414 0415 0424 0429 0430 0433 0434 0435 0438 0442 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 Configuration 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 COMPA01 1 DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 3 5

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# @A340 SERVICE BULLETIN

MATERIAL QTY PER A/C SEE NOTES Component COMPA02 1 Consumable CMLA01 1 B. CONCURRENT REQUIREMENTS None C. REASON (1) History A rod manufacturing process defect has been identified at TAC that could have led to deliver rods with cracks (crimped end of the rod only). (2) Objective/Action This Inspection Service Bulletin (ISB) requires to inspect some rods in the belly fairing. Those rods can be manufactured by either SARMA-SKF or by TAC. - If they are manufactured by SARMA-SKF, no further action is required. - If they are manufactured by TAC, it is mandatory within 6 years from the ISB issuance to perform a Non Destructive Test (NDT) inspection at the crimped end of the rod body. Cracked TAC rods must be replaced. (3) Advantages Accomplishment of this ISB will prevent any cracks on rods installed on the belly fairing. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 534185-832-801-001: Inspection (1) Do a One Time Detailed Inspection of the Rods Task 534185-832-802-001: Inspection (1) Do a HFEC Inspection of the TAC Rods (2) Replace the Upper Rods of the Belly Fairing Structure at FR39 (3) Replace the Lateral Rods of the Belly Fairing Structure at FR39 (4) Replace the Lateral Rods of the Belly Fairing Structure at FR47
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 4 5

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# @A340 SERVICE BULLETIN (5) Replace the Central Rod of the Belly Fairing Structure at FR47 (6) Replace the Upper Rods of the Belly Fairing Structure at FR53.2 (7) Replace the Lateral Rods of the Belly Fairing Structure at FR53.2 (8) Replace the Center Rods of the Belly Fairing Structure at FR53.2 (9) Replace the Upper Rods of the Belly Fairing Structure at FR53.4 (10) Replace the Lateral Rods of the Belly Fairing Structure at FR53.4 (11) Replace the Lateral Rods of the Belly Fairing Structure at FR53.9 (12) Replace the Rods of the Supports of the MLG Door Uplock at FR48 E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. (2) Accomplishment Timescale Accomplishment of this Service Bulletin is expected to be rendered mandatory by the issue of an Airworthiness Directive (AD) published by the European Aviation Safety Agency (EASA). It is anticipated that the AD will confirm the thresholds given below but reference should be made to the AD for confirmation of the mandated accomplishment timescale. COMPLIANCE TIME (whichever occurs first) CONDITION ACTION THRESHOLD GRACE PERIOD REPETITIVE INTERVAL NOT TO EXCEED (whichever occurs first) CONF 001 Inspect in accordance with SUBTASK 534185-832-001 001 Do a One Time Detailed Inspection of the Rods . Not later than six years from SB issuance - Not applicable

TAC rod found or manufacturer cannot be identified Do a HFEC inspection of the rod in accordance with SUBTASK 534185-832-003 001 Do a HFEC Inspection of the TAC Rods Not later than six years from SB issuance (See NOTE) - Not applicable

Other manufacturer rod found. No further action

- - -
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 5 5

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# @A340 SERVICE BULLETIN
COMPLIANCE TIME (whichever occurs first) CONDITION ACTION THRESHOLD GRACE PERIOD REPETITIVE INTERVAL NOT TO EXCEED (whichever occurs first) If the manufacturer of the new rod to be installed is not TAC, replace the rod in accordance with SUBTASK 534185-833-001 001 Replace the Upper Rods of the Belly Fairing Structure at FR39 thru SUBTASK 534185-833-011 001 Replace the Rods of the Supports of the MLG Door Uplock at FR48 Crack(s) found

If the manufacturer of the new rod to be installed is TAC, do a HFEC inspection of the rod. - In case of

finding, discard the rod and do the same with another rod. - If no findings,

replace the rod in accordance with SUBTASK 534185-833-001 001 Replace the Upper Rods of the Belly Fairing Structure at FR39 thru SUBTASK 534185-833-011 001 Replace the Rods of the Supports of the MLG Door Uplock at FR48 Before next flight

- Not applicable

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 6 5

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# @A340 SERVICE BULLETIN
COMPLIANCE TIME (whichever occurs first) CONDITION ACTION THRESHOLD GRACE PERIOD REPETITIVE INTERVAL NOT TO EXCEED (whichever occurs first) No crack found. No further action

- - - NOTE : It is not necessary to perform the HFEC inspection on TAC rods immediately after identification of the rod manufacturer. Aircraft can go back into service and the HFEC inspection can be performed later. However, HFEC inspection must be performed within six years from the ISB revision 00 issuance. NOTE: We recommend to perform the preliminary detailed inspection at the first C Check from SB issuance date, in order to have time to contact AIRBUS Material, Logistics and suppliers (SMM) and to ensure all rods (and B/E Aerospace for associated hardware) availability during the month where the HFEC inspection will be performed on the aircraft. F. APPROVAL Approved under EASA 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. Task 534185-832-801-001: Inspection Get Access 3.00 On Aircraft Do a One Time Detailed Inspection of the Rods 0.25 Close-Up 4.00 TOTAL MANHOURS 7.25 ELAPSED TIME (HOURS) 7.25 NOTE : The values given for the inspections are valid only for one rod.

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 7 5

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# @A340 SERVICE BULLETIN
Task 534185-832-802-001: Inspection Get Access 3.00 On Aircraft Do a HFEC Inspection of the TAC Rods 0.50 Replace the Upper Rods of the Belly Fairing Structure at FR39 0.50 Replace the Lateral Rods of the Belly Fairing Structure at FR39 0.50 Replace the Lateral Rods of the Belly Fairing Structure at FR47 0.50 Replace the Central Rod of the Belly Fairing Structure at FR47 0.50 Replace the Upper Rods of the Belly Fairing Structure at FR53.2 0.50 Replace the Lateral Rods of the Belly Fairing Structure at FR53.2 0.50 Replace the Center Rods of the Belly Fairing Structure at FR53.2 0.50 Replace the Upper Rods of the Belly Fairing Structure at FR53.4 0.50 Replace the Lateral Rods of the Belly Fairing Structure at FR53.4 0.50 Replace the Lateral Rods of the Belly Fairing Structure at FR53.9 0.50 Replace the Rods of the Supports of the MLG Door Uplock at FR48 0.50 Close-Up 4.00 TOTAL MANHOURS 13.00 ELAPSED TIME (HOURS) 13.00 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 06-41-53 12-34-24 20-11-11 20-21-11 32-12-00 53-35-11 53-35-13 Elec. Std. Practices Manual (ESPM) 20-55-00 Non Destructive Test Manual (NTM) 51-10-08 Standards Manual (SM) Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-49-00

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# @A340 SERVICE BULLETIN
K. PUBLICATION AFFECTED None L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

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# @A340 SERVICE BULLETIN

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# @A340 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses 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 COMPA01 AIRBUS Material, Logistics and Suppliers Weg beim Jaeger 150 D-22335 Hamburg Germany For ordering by internet: http://spares.airbus.com For ordering of single spares by fax: +49 40 50 76 40 13 E-Mail : ifd.spares@airbus.com Component COMPA02 BAE Aerospoace 10000 NW 15th Terrace Miami, FL 33172 USA Tel : EMEA : +49 (0) 40 822 285 31500 US : +1 305 925 2600 ASIA : +1 310 900 1300 Fax : EMEA : +49 (0) 40 822 285 31010 US : +1 305 507 7191 ASIA : +1 310 819 1200 Sita : MIAMMCR or contact your daily sales contact E-Mail : AOGdesk_CMG@baeaerospace.com (2) Price and Availability No AIRBUS kit will be provided. Parts required to accomplish this Service Bulletin are to be purchased by a Spares Purchase Order. B. INDUSTRY SUPPORT INFORMATION AIRBUS will provide the operator supplied AIRBUS parts at no charge for those aircraft with findings further to inspection as per this Service Bulletin. AIRBUS will reimburse the operator supplied standard hardware parts for those aircraft with findings further to inspection as per this Service Bulletin. AIRBUS will credit the manhours indicated in this Service Bulletin for inspections that are performed on aircraft in warranty at the time of such inspection. Claims for labor allowance should be received not later than 90 days after completion of the last affected warranted aircraft. DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 11 5

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# @A340 SERVICE BULLETIN
C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Brush Consistency 09-013B As required Corrosion Preventive Temporary Protective Compound 15-005A As required (2) Components NOTE : We recommend to perform the preliminary detailed inspection at the first C Check from SB issuance date, in order to have time to contact AIRBUS Material, Logistics and suppliers (SMM) and to ensure all rods (and B/E Aerospace for associated hardware) availability during the month where the HFEC inspection will be performed on the aircraft. Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 F0003010400100 2 ROD 2 F0003010400300 2 ROD 3 F0003010400400 2 ROD 4 F0003010400500 4 ROD 5 F0003010400700 2 ROD 6 F0003010400800 2 ROD 7 F0003010400900 1 ROD 8 F0003010401100 2 ROD 9 F0003010401200 2 ROD 10 F0003010401400 2 ROD NOTE: The necessary quantity of rods depends on the inspection results. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 15 MS24665-153 36 PIN 18 MS24665-300 6 PIN

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 12 5

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# @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 necessary quantity of pins depends on the inspection results. (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 13 5

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# @A340 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 534185-832-801-001 - Inspection 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. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data Zone 190 Manpower TOTAL MANHOURS 7.25 ELAPSED TIME (HOURS) 7.25 A. GENERAL (1) Subtask 534185-839-001-001 - 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 534185-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 15 5

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# @A340 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 12-34-24-860-802 Task 32-12-00-010-801 Task 53-35-11-000-801 Task 53-35-13-000-801 Task 53-35-13-000-802 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Open the MLG doors (Refer to AMM Task 32-12-00-010-801). (c) Remove the following belly fairing access panels : (Refer to AMM 06-41-53, Page Block 001, AMM Task 53-35-11-000-801, AMM Task 53-35-13-000-801 and AMM Task 53-35-13-000-802). 191BB, 191CB, 191QB, 192BB, 192CB, 192QB, 195CB or 195AB, 196GB or 196AB, 197BB, 197EB, 197GB, 197HB, 198BB, 198EB, 198GB and 198HB (d) Put access platform(s) in position. (2) Subtask 534185-020-001-001 - Remove the Aft Fillet Fairing from LH side for Access Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 53-35-11-000-802 Fig. A-FBDAA Remove/Install the Aft Fillet Fairing for access Sheet 01
(a) Remove : Fig. A-FBDAA (Refer to AMM Task 53-35-11-000-802) 1 Aft Fillet Fairing Item (30) Retain

(3) Subtask 534185-020-002-001 - Remove the Aft Fillet Fairing from RH side for Access Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 53-35-11-000-802

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 16 5

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# @A340 SERVICE BULLETIN

References Fig. A-FBDAA Remove/Install the Aft Fillet Fairing for access Sheet 01
(a) Remove : Fig. A-FBDAA (Refer to AMM Task 53-35-11-000-802) 1 Aft Fillet Fairing Item (31 ) Retain C. PROCEDURE (1) Subtask 534185-832-001-001 - Do a One Time Detailed Inspection of the Rods Work Zones and Access Panels Zone Access/Work location 190 Manpower Resources Manhours 0.25 Minimum number of person 1 Subtask elapsed time 0.25 Skills NON SPECIFIC References Fig. A-FBAAA Area to be Inspected Sheet 01 Sheet 02 Sheet 03 Sheet 04 Fig. A-FBBAA Flow Chart Sheet 01 Sheet 02 (a) For the inspection area, refer to Fig. A-FBAAA

. (b) Do a one time detailed inspection of the rods. Refer to Fig. A-FBBAA

. 1 If the manufacturer of the rod is TAC or if the manufacturer cannot be identified, go to SUBTASK 534185-832-003 001 Do a HFEC Inspection of the TAC Rods or go to SUBTASK 534185-942-001 001 Close-up and release your aircraft, if you intend to do the HFEC inspection later (SUBTASK 534185-832-003 001) but within 6 years from the ISB revision 00 issuance. NOTE : We recommend to perform the preliminary detailed inspection at the first C Check from SB issuance date, in order to have time to contact AIRBUS Material, Logistics and suppliers (SMM) and to ensure all rods (and B/E Aerospace for associated hardware) availability during the month where the DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 17 5

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# @A340 SERVICE BULLETIN HFEC inspection will be performed on the aircraft. 2 If the manufacturer of the rod is not TAC, no further action is required. (c) For the inspection report, refer to Appendix 01 . D. TEST None E. CLOSE-UP (1) Subtask 534185-420-001-001 - Install the Aft Fillet Fairing at LH side Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 53-35-11-400-802 Fig. A-FBDAA Remove/Install the Aft Fillet Fairing for access Sheet 01
(a) Install : Fig. A-FBDAA (Refer to AMM Task 53-35-11-400-802) 1 Aft Fillet Fairing Item (30) Retained at removal (2) Subtask 534185-420-002-001 - Install the Aft Fillet Fairing at RH side Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 53-35-11-400-802 Fig. A-FBDAA Remove/Install the Aft Fillet Fairing for access Sheet 01
(a) Install : Fig. A-FBDAA (Refer to AMM Task 53-35-11-400-802) 1 Aft Fillet Fairing Item (31 ) Retained at removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 18 5

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# @A340 SERVICE BULLETIN (3) Subtask 534185-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 32-12-00-410-801 Task 53-35-11-000-801 Task 53-35-13-000-801 Task 53-35-13-000-802 (a) Make sure that the work areas are clean and clear of tools and any other items of equipment. (b) Remove the access platform(s). (c) Install the following belly fairing access panels : (Refer to AMM 06-41-53, Page Block 001, AMM Task 53-35-11-000-801, AMM Task 53-35-13-000-801 and AMM Task 53-35-13-000-802). 191BB, 191CB, 191QB, 192BB, 192CB, 192QB, 195CB or 195AB, 196GB or 196AB, 197BB, 197EB, 197GB, 197HB, 198BB, 198EB, 198GB and 198HB (d) Close the MLG doors (Refer to AMM Task 32-12-00-410-801). (e) Restore the systems and the aircraft to normal operating conditions.

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 19 5

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# @A340 SERVICE BULLETIN

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# @A340 SERVICE BULLETIN Task 534185-832-802-001 - Inspection 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. IN CASE OF CONTAMINATION REFER TO ESPM 20-55-00. Task Associated Data Zone 190 Manpower TOTAL MANHOURS 13.00 ELAPSED TIME (HOURS) 13.00 A. GENERAL (1) Subtask 534185-839-002-001 - Administrative Manpower Resources Skills NON SPECIFIC Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. (2) Subtask 534185-910-002-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 21 5

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# @A340 SERVICE BULLETIN
Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Corrosion Inhibiting Brush Consistency 09-013B As required Corrosion Preventive Temporary Protective Compound 15-005A As required

References Aircraft Maintenance Manual (AMM) Task 20-11-11-911-803 Task 20-21-11-911-801 Structural Repair Manual (SRM) 51-23-12 51-42-00 51-43-00 51-49-00 (a) Remove and install the fasteners (Refer to SRM 51-42-00). (b) For alternative and substitute fasteners, refer to SRM 51-43-00. (c) Torque the standard threaded fasteners (Refer to SRM 51-49-00 and AMM Task 20-21-11-911-801). (d) Renew the protective finish with : Corrosion Preventive Temporary Protective Compound 15-005A As required

(Refer to SRM 51-23-12) (e) On the head of the fasteners apply : Corrosion Inhibiting Brush Consistency 09-013B As required (f) Secure the rod ends with lock wire (Refer to AMM Task 20-11-11-911-803). B. PREPARATION (1) Subtask 534185-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 22 5

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# @A340 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 12-34-24-860-802 Task 32-12-00-010-801 Task 53-35-11-000-801 Task 53-35-13-000-801 Task 53-35-13-000-802 (a) Make sure that the aircraft is electrically grounded (Refer to AMM Task 12-34-24-860-802). (b) Open the MLG doors (Refer to AMM Task 32-12-00-010-801). (c) Remove the following belly fairing access panels : (Refer to AMM 06-41-53, Page Block 001, AMM Task 53-35-11-000-801, AMM Task 53-35-13-000-801 and AMM Task 53-35-13-000-802). 191BB, 191CB, 191QB, 192BB, 192CB, 192QB, 195CB or 195AB, 196GB or 196AB, 197BB, 197EB, 197GB, 197HB, 198BB, 198EB, 198GB and 198HB (d) Put access platform(s) in position. (2) Subtask 534185-020-003-001 - Remove the Aft Fillet Fairing from LH side for Access Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 53-35-11-000-802 Fig. A-FBDAA Remove/Install the Aft Fillet Fairing for access Sheet 01
(a) Remove : Fig. A-FBDAA (Refer to AMM Task 53-35-11-000-802) 1 Aft Fillet Fairing Item (30) Retain

(3) Subtask 534185-020-004-001 - Remove the Aft Fillet Fairing from RH side for Access Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 53-35-11-000-802

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 23 5

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# @A340 SERVICE BULLETIN

References Fig. A-FBDAA Remove/Install the Aft Fillet Fairing for access Sheet 01
(a) Remove : Fig. A-FBDAA (Refer to AMM Task 53-35-11-000-802) 1 Aft Fillet Fairing Item (31 ) Retain C. PROCEDURE (1) Subtask 534185-832-003-001 - Do a HFEC Inspection of the TAC Rods Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills NON DESTRUCTIVE TESTING References Non Destructive Test Manual (NTM) 51-10-08 Fig. A-FBAAA Area to be Inspected Sheet 01 Sheet 02 Sheet 03 Sheet 04 Fig. A-FBBAA Flow Chart Sheet 01 Sheet 02 (a) For the inspection area, refer to Fig. A-FBAAA

. (b) Do a HFEC inspection of the TAC rods as per NTM 51-10-08. Refer to Fig. A-FBBAA

. 1 If no crack is found, no further action is required. 2 If crack is found, do the following steps. (c) For the inspection report, refer to Appendix 01 . (2) Subtask 534185-833-001-001 - Replace the Upper Rods of the Belly Fairing Structure at FR39 Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 39

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 24 5

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# @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 COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 4 F0003010400500 2 ROD NOTE: The necessary quantity of rods depends on the inspection results. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 15 MS24665-153 4 PIN NOTE: The necessary quantity of pins depends on the inspection results. References Fig. A-FBCAA Replacement of the rods Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 (a) Remove from LH side : Fig. A-FBCAA Sheet 03, Detail F 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 2 Washer Item (13) Retain 2 Washer Item (14) Retain 2 Pin Item (15) Discard 2 Bush Item (16) Retain 2 Bush Item (17) Retain 1 Rod Item (4) Discard
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 25 5

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# @A340 SERVICE BULLETIN (b) Install on LH side : Fig. A-FBCAA Sheet 03, Detail F NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400500 Item 4 2 Bush Item (16) Retained at removal 2 Bush Item (17) Retained at removal 2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 2 Washer Item (13) Retained at removal 2 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15 (c) Remove from RH side : Fig. A-FBCAA Sheet 03, Detail F 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 2 Washer Item (13) Retain 2 Washer Item (14) Retain 2 Pin Item (15) Discard 2 Bush Item (16) Retain 2 Bush Item (17) Retain 1 Rod Item (4) Discard

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 26 5

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# @A340 SERVICE BULLETIN (d) Install on RH side : Fig. A-FBCAA Sheet 03, Detail F NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400500 Item 4 2 Bush Item (16) Retained at removal 2 Bush Item (17) Retained at removal 2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 2 Washer Item (13) Retained at removal 2 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15

(3) Subtask 534185-833-002-001 - Replace the Lateral Rods of the Belly Fairing Structure at FR39 Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 39 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 F0003010400100 2 ROD NOTE: The necessary quantity of rods depends on the inspection results. DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 27 5

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# @A340 SERVICE BULLETIN
Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 15 MS24665-153 4 PIN NOTE: The necessary quantity of pins depends on the inspection results. References Fig. A-FBCAA Replacement of the rods Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 (a) Remove from LH side : Fig. A-FBCAA Sheet 03, Detail F 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 2 Washer Item (13) Retain 2 Washer Item (14) Retain 2 Pin Item (15) Discard 2 Bush Item (16) Retain 2 Bush Item (17) Retain 1 Rod Item (1 ) Discard (b) Install on LH side : Fig. A-FBCAA Sheet 03, Detail F NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400100 Item 1 2 Bush Item (16) Retained at removal 2 Bush Item (17) Retained at removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 28 5

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# @A340 SERVICE BULLETIN
2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 2 Washer Item (13) Retained at removal 2 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15 (c) Remove from RH side : Fig. A-FBCAA Sheet 03, Detail F 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 2 Washer Item (13) Retain 2 Washer Item (14) Retain 2 Pin Item (15) Discard 2 Bush Item (16) Retain 2 Bush Item (17) Retain 1 Rod Item (1 ) Discard (d) Install on RH side : Fig. A-FBCAA Sheet 03, Detail F NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400100 Item 1 2 Bush Item (16) Retained at removal 2 Bush Item (17) Retained at removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 29 5

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# @A340 SERVICE BULLETIN
2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 2 Washer Item (13) Retained at removal 2 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15

(4) Subtask 534185-833-003-001 - Replace the Lateral Rods of the Belly Fairing Structure at FR47 Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 47 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 8 F0003010401100 2 ROD NOTE: The necessary quantity of rods depends on the inspection results. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 15 MS24665-153 2 PIN 18 MS24665-300 2 PIN NOTE: The necessary quantity of pins depends on the inspection results.

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 30 5

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# @A340 SERVICE BULLETIN

References Fig. A-FBCAA Replacement of the rods Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 (a) Remove from LH side : Fig. A-FBCAA Sheet 04, Detail G 1 Bolt Item (20) Retain 1 Bolt Item (21) Retain 2 Nut Item (19) Retain 2 Washer Item (22) Retain 2 Washer Item (23) Retain 1 Pin Item (15) Discard 1 Pin Item (18) Discard 1 Bush Item (24) Retain 1 Bush Item (25) Retain 1 Bush Item (26) Retain 1 Bush Item (27) Retain 1 Rod Item (8) Discard (b) Install on LH side : Fig. A-FBCAA Sheet 04, Detail G NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010401100 Item 8 1 Bush Item (24) Retained at removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 31 5

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# @A340 SERVICE BULLETIN
1 Bush Item (25) Retained at removal 1 Bush Item (26) Retained at removal 1 Bush Item (27) Retained at removal 1 Bolt Item (20) Retained at removal 1 Bolt Item (21) Retained at removal 2 Nut Item (19) Retained at removal 2 Washer Item (22) Retained at removal 2 Washer Item (23) Retained at removal 1 Pin-Cotter MS24665-153 Item 15 1 Pin-Cotter MS24665-300 Item 18 (c) Remove from RH side : Fig. A-FBCAA Sheet 04, Detail G 1 Bolt Item (20) Retain 1 Bolt Item (21) Retain 2 Nut Item (19) Retain 2 Washer Item (22) Retain 2 Washer Item (23) Retain 1 Pin Item (15) Discard 1 Pin Item (18) Discard 1 Bush Item (24) Retain 1 Bush Item (25) Retain

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 32 5

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# @A340 SERVICE BULLETIN
1 Bush Item (26) Retain 1 Bush Item (27) Retain 1 Rod Item (8) Discard (d) Install on RH side : Fig. A-FBCAA Sheet 04, Detail G NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010401100 Item 8 1 Bush Item (24) Retained at removal 1 Bush Item (25) Retained at removal 1 Bush Item (26) Retained at removal 1 Bush Item (27) Retained at removal 1 Bolt Item (20) Retained at removal 1 Bolt Item (21) Retained at removal 2 Nut Item (19) Retained at removal 2 Washer Item (22) Retained at removal 2 Washer Item (23) Retained at removal 1 Pin-Cotter MS24665-153 Item 15 1 Pin-Cotter MS24665-300 Item 18

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 33 5

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# @A340 SERVICE BULLETIN (5) Subtask 534185-833-004-001 - Replace the Central Rod of the Belly Fairing Structure at FR47 Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 47 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 7 F0003010400900 1 ROD NOTE: The necessary quantity of rods depends on the inspection results. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 15 MS24665-153 2 PIN NOTE: The necessary quantity of pins depends on the inspection results. References Fig. A-FBCAA Replacement of the rods Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 (a) Remove : Fig. A-FBCAA Sheet 03, Detail F 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 2 Washer Item (13) Retain 2 Washer Item (14) Retain 2 Pin Item (15) Discard
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 34 5

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# @A340 SERVICE BULLETIN
2 Bush Item (16) Retain 2 Bush Item (17) Retain 1 Rod Item (7) Discard (b) Install : Fig. A-FBCAA Sheet 03, Detail F NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400900 Item 7 2 Bush Item (16) Retained at removal 2 Bush Item (17) Retained at removal 2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 2 Washer Item (13) Retained at removal 2 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15

(6) Subtask 534185-833-005-001 - Replace the Upper Rods of the Belly Fairing Structure at FR53.2 Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 53.2 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 35 5

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# @A340 SERVICE BULLETIN
Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 10 F0003010401400 2 ROD NOTE: The necessary quantity of rods depends on the inspection results. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 15 MS24665-153 4 PIN NOTE: The necessary quantity of pins depends on the inspection results. References Fig. A-FBCAA Replacement of the rods Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 (a) Remove from LH side : Fig. A-FBCAA Sheet 03, Detail F 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 2 Washer Item (13) Retain 2 Washer Item (14) Retain 2 Pin Item (15) Discard 2 Bush Item (16) Retain 2 Bush Item (17) Retain 1 Rod Item (10) Discard (b) Install on LH side : Fig. A-FBCAA Sheet 03, Detail F NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 36 5

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# @A340 SERVICE BULLETIN

1 Rod F0003010401400 Item 10 2 Bush Item (16) Retained at removal 2 Bush Item (17) Retained at removal 2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 2 Washer Item (13) Retained at removal 2 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15 (c) Remove from RH side : Fig. A-FBCAA Sheet 03, Detail F 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 2 Washer Item (13) Retain 2 Washer Item (14) Retain 2 Pin Item (15) Discard 2 Bush Item (16) Retain 2 Bush Item (17) Retain 1 Rod Item (10) Discard (d) Install on RH side : Fig. A-FBCAA Sheet 03, Detail F NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010401400 Item 10 DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 37 5

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# @A340 SERVICE BULLETIN
2 Bush Item (16) Retained at removal 2 Bush Item (17) Retained at removal 2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 2 Washer Item (13) Retained at removal 2 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15

(7) Subtask 534185-833-006-001 - Replace the Lateral Rods of the Belly Fairing Structure at FR53.2 Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 53.2 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 5 F0003010400700 2 ROD NOTE: The necessary quantity of rods depends on the inspection results. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 18 MS24665-300 4 PIN NOTE: The necessary quantity of pins depends on the inspection results.

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 38 5

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# @A340 SERVICE BULLETIN

References Fig. A-FBCAA Replacement of the rods Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 (a) Remove from LH side : Fig. A-FBCAA Sheet 04, Detail H 2 Bolt Item (21) Retain 2 Nut Item (19) Retain 4 Washer Item (22) Retain 2 Pin Item (18) Discard 2 Bush Item (26) Retain 2 Bush Item (27) Retain 1 Rod Item (5) Discard (b) Install on LH side Fig. A-FBCAA Sheet 04, Detail H NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400700 Item 5 2 Bush Item (26) Retained at removal 2 Bush Item (27) Retained at removal 2 Bolt Item (21) Retained at removal 2 Nut Item (19) Retained at removal 4 Washer Item (22) Retained at removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 39 5

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# @A340 SERVICE BULLETIN

2 Pin-Cotter MS24665-300 Item 18 (c) Remove from RH side : Fig. A-FBCAA Sheet 04, Detail H 2 Bolt Item (21) Retain 2 Nut Item (19) Retain 4 Washer Item (22) Retain 2 Pin Item (18) Discard 2 Bush Item (26) Retain 2 Bush Item (27) Retain 1 Rod Item (5) Discard (d) Install on RH side Fig. A-FBCAA Sheet 04, Detail H NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400700 Item 5 2 Bush Item (26) Retained at removal 2 Bush Item (27) Retained at removal 2 Bolt Item (21) Retained at removal 2 Nut Item (19) Retained at removal 4 Washer Item (22) Retained at removal 2 Pin-Cotter MS24665-300 Item 18

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 40 5

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# @A340 SERVICE BULLETIN (8) Subtask 534185-833-007-001 - Replace the Center Rods of the Belly Fairing Structure at FR53.2 Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 53.2 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 6 F0003010400800 2 ROD NOTE: The necessary quantity of rods depends on the inspection results. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 15 MS24665-153 4 PIN NOTE: The necessary quantity of pins depends on the inspection results. References Fig. A-FBCAA Replacement of the rods Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 (a) Remove from LH side : Fig. A-FBCAA Sheet 05, Detail J 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 4 Washer Item (13) Retain 2 Pin Item (15) Discard 2 Bush Item (17) Retain
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 41 5

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# @A340 SERVICE BULLETIN
2 Bush Item (16) Retain 1 Rod Item (6) Discard (b) Install on LH side : Fig. A-FBCAA Sheet 05, Detail J NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400800 Item 6 2 Bush Item (17) Retained at removal 2 Bush Item (16) Retained at removal 2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 4 Washer Item (13) Retained at removal 2 Pin-Cotter MS24665-153 Item 15 (c) Remove from RH side : Fig. A-FBCAA Sheet 05, Detail J 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 4 Washer Item (13) Retain 2 Pin Item (15) Discard 2 Bush Item (17) Retain 2 Bush Item (16) Retain 1 Rod Item (6) Discard

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 42 5

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# @A340 SERVICE BULLETIN (d) Install on RH side : Fig. A-FBCAA Sheet 05, Detail J NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400800 Item 6 2 Bush Item (17) Retained at removal 2 Bush Item (16) Retained at removal 2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 4 Washer Item (13) Retained at removal 2 Pin-Cotter MS24665-153 Item 15

(9) Subtask 534185-833-008-001 - Replace the Upper Rods of the Belly Fairing Structure at FR53.4 Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 53.4 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 3 F0003010400400 2 ROD NOTE: The necessary quantity of rods depends on the inspection results.

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 43 5

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# @A340 SERVICE BULLETIN
Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 15 MS24665-153 4 PIN NOTE: The necessary quantity of pins depends on the inspection results. References Fig. A-FBCAA Replacement of the rods Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 (a) Remove from LH side : Fig. A-FBCAA Sheet 05, Detail K 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 4 Washer Item (14) Retain 2 Pin Item (15) Discard 2 Bush Item (17) Retain 2 Bush Item (28) Retain 1 Rod Item (3) Discard (b) Install on LH side : Fig. A-FBCAA Sheet 05, Detail K NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400400 Item 3 2 Bush Item (17) Retained at removal 2 Bush Item (28) Retained at removal 2 Bolt Item (11) Retained at removal DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 44 5

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# @A340 SERVICE BULLETIN
2 Nut Item (12) Retained at removal 4 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15 (c) Remove from RH side : Fig. A-FBCAA Sheet 05, Detail K 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 4 Washer Item (14) Retain 2 Pin Item (15) Discard 2 Bush Item (17) Retain 2 Bush Item (28) Retain 1 Rod Item (3) Discard (d) Install on RH side : Fig. A-FBCAA Sheet 05, Detail K NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400400 Item 3 2 Bush Item (17) Retained at removal 2 Bush Item (28) Retained at removal 2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 4 Washer Item (14) Retained at removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 45 5

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# @A340 SERVICE BULLETIN

2 Pin-Cotter MS24665-153 Item 15

(10) Subtask 534185-833-009-001 - Replace the Lateral Rods of the Belly Fairing Structure at FR53.4 Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 53.4 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 2 F0003010400300 2 ROD NOTE: The necessary quantity of rods depends on the inspection results. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 15 MS24665-153 4 PIN NOTE: The necessary quantity of pins depends on the inspection results. References Fig. A-FBCAA Replacement of the rods Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 (a) Remove from LH side : Fig. A-FBCAA Sheet 05, Detail K 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 4 Washer Item (14) Retain 2 Pin Item (15) Discard
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 46 5

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# @A340 SERVICE BULLETIN
2 Bush Item (17) Retain 2 Bush Item (28) Retain 1 Rod Item (2) Discard (b) Install at LH side : Fig. A-FBCAA Sheet 05, Detail K NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400300 Item 2 2 Bush Item (17) Retained at removal 2 Bush Item (28) Retained at removal 2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 4 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15 (c) Remove from RH side : Fig. A-FBCAA Sheet 05, Detail K 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 4 Washer Item (14) Retain 2 Pin Item (15) Discard 2 Bush Item (17) Retain 2 Bush Item (28) Retain 1 Rod Item (2) Discard
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 47 5

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# @A340 SERVICE BULLETIN (d) Install at RH side : Fig. A-FBCAA Sheet 05, Detail K NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400300 Item 2 2 Bush Item (17) Retained at removal 2 Bush Item (28) Retained at removal 2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 4 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15

(11) Subtask 534185-833-010-001 - Replace the Lateral Rods of the Belly Fairing Structure at FR53.9 Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 53.9 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 4 F0003010400500 2 ROD NOTE: The necessary quantity of rods depends on the inspection results.

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 48 5

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# @A340 SERVICE BULLETIN
Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 15 MS24665-153 4 PIN NOTE: The necessary quantity of pins depends on the inspection results. References Fig. A-FBCAA Replacement of the rods Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06 (a) Remove from LH side : Fig. A-FBCAA Sheet 03, Detail F 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 2 Washer Item (13) Retain 2 Washer Item (14) Retain 2 Pin Item (15) Discard 2 Bush Item (16) Retain 2 Bush Item (17) Retain 1 Rod Item (4) Discard (b) Install at LH side : Fig. A-FBCAA Sheet 03, Detail F NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400500 Item 4 2 Bush Item (16) Retained at removal 2 Bush Item (17) Retained at removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 49 5

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# @A340 SERVICE BULLETIN
2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 2 Washer Item (13) Retained at removal 2 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15 (c) Remove from RH side : Fig. A-FBCAA Sheet 03, Detail F 2 Bolt Item (11) Retain 2 Nut Item (12) Retain 2 Washer Item (13) Retain 2 Washer Item (14) Retain 2 Pin Item (15) Discard 2 Bush Item (16) Retain 2 Bush Item (17) Retain 1 Rod Item (4) Discard (d) Install at RH side : Fig. A-FBCAA Sheet 03, Detail F NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010400500 Item 4 2 Bush Item (16) Retained at removal 2 Bush Item (17) Retained at removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 50 5

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# @A340 SERVICE BULLETIN
2 Bolt Item (11) Retained at removal 2 Nut Item (12) Retained at removal 2 Washer Item (13) Retained at removal 2 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15

(12) Subtask 534185-833-011-001 - Replace the Rods of the Supports of the MLG Door Uplock at FR48 Work Zones and Access Panels Zone Access/Work location 190 Work location Frame 48 Manpower Resources Manhours 0.50 Minimum number of person 1 Subtask elapsed time 0.50 Skills AIRFRAME Material necessary to do the job Component COMPA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 9 F0003010401200 2 ROD NOTE: The necessary quantity of rods depends on the inspection results. Component COMPA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 15 MS24665-153 4 PIN NOTE: The necessary quantity of pins depends on the inspection results. References Fig. A-FBCAA Replacement of the rods Sheet 01 Sheet 02 Sheet 03 Sheet 04 Sheet 05 Sheet 06
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 51 5

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# @A340 SERVICE BULLETIN (a) Remove from LH side : Fig. A-FBCAA Sheet 06, Detail L 1 Bolt Item (11) Retain 1 Bolt Item (21) Retain 2 Nut Item (12) Retain 2 Washer Item (13) Retain 2 Washer Item (14) Retain 2 Pin Item (15) Discard 1 Bush Item (17) Retain 1 Bush Item (28) Retain 1 Rod Item (9) Discard (b) Install on LH side : Fig. A-FBCAA Sheet 06, Detail L NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010401200 Item 9 1 Bush Item (17) Retained at removal 1 Bush Item (28) Retained at removal 1 Bolt Item (11) Retained at removal 1 Bolt Item (21) Retained at removal 2 Nut Item (12) Retained at removal 2 Washer Item (13) Retained at removal

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 52 5

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# @A340 SERVICE BULLETIN
2 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15 (c) Remove from RH side : Fig. A-FBCAA Sheet 06, Detail L 1 Bolt Item (11) Retain 1 Bolt Item (21) Retain 2 Nut Item (12) Retain 2 Washer Item (13) Retain 2 Washer Item (14) Retain 2 Pin Item (15) Discard 1 Bush Item (17) Retain 1 Bush Item (28) Retain 1 Rod Item (9) Discard (d) Install on RH side : Fig. A-FBCAA Sheet 06, Detail L NOTE: For the installation of the rod, it has to be adjusted to the correct length and secured with lock wire on both sides then you can torque the fasteners. 1 Rod F0003010401200 Item 9 1 Bush Item (17) Retained at removal 1 Bush Item (28) Retained at removal 1 Bolt Item (11) Retained at removal 1 Bolt Item (21) Retained at removal 2 Nut Item (12) Retained at removal DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 53 5

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# @A340 SERVICE BULLETIN
2 Washer Item (13) Retained at removal 2 Washer Item (14) Retained at removal 2 Pin-Cotter MS24665-153 Item 15 D. TEST None E. CLOSE-UP (1) Subtask 534185-420-003-001 - Install the Aft Fillet Fairing at LH side Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 53-35-11-400-802 Fig. A-FBDAA Remove/Install the Aft Fillet Fairing for access Sheet 01
(a) Install : Fig. A-FBDAA (Refer to AMM Task 53-35-11-400-802) 1 Aft Fillet Fairing Item (30) Retained at removal (2) Subtask 534185-420-004-001 - Install the Aft Fillet Fairing at RH side Manpower Resources Skills AIRFRAME References Aircraft Maintenance Manual (AMM) Task 53-35-11-400-802 Fig. A-FBDAA Remove/Install the Aft Fillet Fairing for access Sheet 01
(a) Install : Fig. A-FBDAA (Refer to AMM Task 53-35-11-400-802)

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 54 5

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# @A340 SERVICE BULLETIN

1 Aft Fillet Fairing Item (31 ) Retained at removal (3) Subtask 534185-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 06-41-53, Page Block 001 Task 32-12-00-410-801 Task 53-35-11-000-801 Task 53-35-13-000-801 Task 53-35-13-000-802 (a) Make sure that the work areas are clean and clear of tools and any other items of equipment. (b) Remove the access platform(s). (c) Install the following belly fairing access panels : (Refer to AMM 06-41-53, Page Block 001, AMM Task 53-35-11-000-801, AMM Task 53-35-13-000-801 and AMM Task 53-35-13-000-802). 191BB, 191CB, 191QB, 192BB, 192CB, 192QB, 195CB or 195AB, 196GB or 196AB, 197BB, 197EB, 197GB, 197HB, 198BB, 198EB, 198GB and 198HB (d) Close the MLG doors (Refer to AMM Task 32-12-00-410-801). (e) Restore the systems and the aircraft to normal operating conditions.

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 55 5

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# @A340 SERVICE BULLETIN

**CONF ALL



### A Z190 FR53.9

FR53.2

FR48

FR37 FR39



### B **C D**  **E**



## A **E**

F_SB_534185_5_BAAA_01_01 Figure A-FBAAA - Sheet 01 Area to be Inspected
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 56 5

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# @A340 SERVICE BULLETIN

**CONF ALL

FR53.4 FR53.9

FR53.2

FR47 FR39



### F
**F F**  **F**

**F**
**F**

**F F**  **F F** 

**F**

**F F** **F F**  **F F**  **F**

**F** 

## B

**C D** 

F_SB_534185_5_BAAA_02_00 Figure A-FBAAA - Sheet 02 Area to be Inspected
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 57 5

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# @A340 SERVICE BULLETIN

**CONF ALL

MANUFACTURER AND PN TO BE IDENTIFIED



## F FR48



### F

LH SIDE SHOWN

RH SIDE SYMMETRICAL 

## E

TYPICAL F_SB_534185_5_BAAA_03_01 

### G

**G**

Figure A-FBAAA - Sheet 03 Area to be Inspected
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 58 5

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# @A340 SERVICE BULLETIN

**CONF ALL

AREA TO BE

TYPICAL CRACK INSPECTED

LOCATION

TYPICAL

F_SB_534185_5_BAAA_04_00 

## G

Figure A-FBAAA - Sheet 04 Area to be Inspected
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 59 5

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# @A340 SERVICE BULLETIN

**CONF ALL

AT THE THRESHOLD GIVEN IN THE PLANNING INFORMATION PARAGRAPH E.2.

THE MANUFACTURER NO YES

REPORT TO AIRBUS REFER TO APPENDIX 01 AS PER NTM 51−10−08 AT THRESHOLD DO A HFEC INSPECTION OF THE ROD GIVEN IN THE PLANNING INFORMATION PARAGRAPH E.2.
NO FURTHER ACTION CRACKS NO YES DO A ONE TIME DETAILED INSPECTION OF THE RODS

IDENTIFY THE PART NUMBER AND THE MANUFACTURER OF THE ROD

OF THE ROD IS TAC OR THE

SEND THE INSPECTION

REPORT TO AIRBUS REFER TO APPENDIX 01

NO FURTHER ACTION SEND THE INSPECTION A−FBBAA SHEET 2 REFER TO FIGURE
QUESTION ACTION FINDING
**NOTE:**

WE RECOMMEND TO PERFORM THE PRELIMINARY DETAILED INSPECTION AT THE FIRST C− CHECK FROM SB ISSUANCE DATE, IN ORDER TO HAVE TIME TO CONTACT AIRBUS MATERIAL, LOGISTICS AND SUPPLIERS (SMM) AND TO ENSURE ALL RODS (AND B/E AEROSPACE FOR ASSOCIATED HARWARE) AVAILABILITY DURING THE MONTH WHEN THE HFEC INSPECTION WILL BE PERFORMED ON THE AIRCRAFT. 

## * *

IT IS NOT NECESSARY TO PERFORM THE HFEC INSPECTION ON TAC RODS IMMEDIATELY AFTER IDENTIFICATION OF THE ROD MANUFACTURER. AIRCRAFT CAN GO BACK INTO SERVICE AND THE HFEC INSPECTION CAN BE PERFORMED LATER. HOWEVER, HFEC INSPECTION MUST BE PERFORMED WITHIN SIX YEARS FROM THE INSPECTION SERVICE BULLETIN REVISION 00 ISSUANCE. MANUFACTURER CANNOT BE IDENTIFIED

F_SB_534185_5_BBAA_01_04 Figure A-FBBAA - Sheet 01 Flow Chart
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 60 5

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# @A340 SERVICE BULLETIN

**CONF ALL

QUESTION ACTION FINDING MANUFACTURER OF NO YES

OF THE NEW ROD DO A HFEC INSPECTION

CRACKS NO YES THE THE NEW ROD TO BE

REPORT TO AIRBUS REFER TO APPENDIX 01

NO FURTHER ACTION SEND THE INSPECTION A−FBBAA SHEET 1

FROM FIGURE

INSTALLED IS TAC

AS PER NTM 51−10−08

AS DESCRIBED IN SUBTASK 534185−833−001−001 THRU 534185−833−011−001 BEFORE NEXT FLIGHT REPLACE THE ROD TO BE INSTALLED AND GET A NEW ONE

DISCARD THE ROD

F_SB_534185_5_BBAA_02_01 Figure A-FBBAA - Sheet 02 Flow Chart
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 61 5

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# @A340 SERVICE BULLETIN

**CONF ALL



### A Z190 FR53.9

FR53.2

FR48

FR37 FR39



### B **C D**  **E**



## A **E**

F_SB_534185_5_BCAA_01_02 Figure A-FBCAA - Sheet 01

Replacement of the rods
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 62 5

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# @A340 SERVICE BULLETIN

**CONF ALL

FR53.4 FR53.9

FR53.2

FR47 FR39



### F
**F F**  **F**

**F F** 

**F F** 

**F** 

## B

**C D**  (1) 1 (4) 4 (4) 4

(1) 1

(8) 8

(8) 8(7)

7 (10) 10 (5) 5

(6) 6
(5) 5 (10) 10 (2) 2 (3) 3(4)

4 (4) 4 (3) 3 (2) 2



### G **K**

**K H** 
**J J** 
**H K**  **K**

**G**

F_SB_534185_5_BCAA_02_02 Figure A-FBCAA - Sheet 02

Replacement of the rods
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 63 5

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# @A340 SERVICE BULLETIN

**CONF ALL FR48

(9) 9

LH SIDE SHOWN RH SIDE SYMMETRICAL 

## E

(11) (14)
(13) (12) 15

(11) (14) (13) (12) (15)

TYPICAL 

## F (15) (17) (16)

(16) (17) 15 

### L

F_SB_534185_5_BCAA_03_02 Figure A-FBCAA - Sheet 03

Replacement of the rods
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 64 5

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# @A340 SERVICE BULLETIN

**CONF ALL

(21) (22)
(22) (19) 18

(21) (22) (22) (19) (18)

TYPICAL (18) (27) (26)

(26) (27) 18 (20) (22)
(23) (19) 15

(21) (22) (23) (19) (18)

TYPICAL (15) (24) (25)

(26) (27) 18



## G

**H** F_SB_534185_5_BCAA_04_01 Figure A-FBCAA - Sheet 04

Replacement of the rods
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 65 5

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# @A340 SERVICE BULLETIN

**CONF ALL

(11) (14)
(14) (12) 15

(11) (14) (14) (12) (15)

TYPICAL (15) (17) (28)

(28) (17) 15 (11) (13)
(13) (12) 15

(11) (13) (13) (12) (15)

TYPICAL (15) (17) (16)

(16) (17) 15



## J

**K** F_SB_534185_5_BCAA_05_01 Figure A-FBCAA - Sheet 05

Replacement of the rods
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 66 5

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# @A340 SERVICE BULLETIN

**CONF ALL

(11)

(13) (12) 15

(21) (14) (13) (12) (15)

TYPICAL (15)

(17) (28) 15


## L (14)

F_SB_534185_5_BCAA_06_01 Figure A-FBCAA - Sheet 06

Replacement of the rods
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 67 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A340 SERVICE BULLETIN

**CONF ALL



### A FR37.4 FR39.1 

### B

(30) (31) LH RH

LH SIDE SHOWN RH SIDE SYMMETRICAL 

## B **A**

F_SB_534185_5_BDAA_01_00 Figure A-FBDAA - Sheet 01 Remove/Install the Aft Fillet Fairing for access
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 68 5

Printed in FRANCE © AIRBUS S.A.S. 2007. All rights reserved.

# @A340 SERVICE BULLETIN Appendix 01 **CONF ALL (1) The result of the inspection, including no findings, replacement or actions to be done, must be forwarded to AIRBUS Department SEES1, on the attached inspection report sheet.

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 1 5

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# @A340 SERVICE BULLETIN Appendix 01

**CONF ALL **INSPECTION REPORT**

DETAIL LH TAC ROD YES SERVICE BULLETIN No. : A/C MSN : FLIGHT CYCLES : FLIGHT HOURS : A340−53−4185

DATE OF INSPECTION : RETURN TO : AIRBUS CUSTOMER SERVICES ENGINEERING − SEES1 FUSELAGE (WB/LR) − VERTICAL TAIL PLANE −

INSPECTION METHOD : CENTER WING BOX (WB/LR) 1 ROUND POINT MAURICE BELLONTE 31707 BLAGNAC CEDEX FRANCE FAX +33 (0)5 61 93 36 14

CRACK FOUND ROD REPLACED ROD LOCATION NO 

## B YES NO YES NO DETAIL RH YES NO 

## B YES NO YES NO DETAIL LH YES NO 

## C YES NO YES NO DETAIL RH YES NO 

## C YES NO YES NO DETAIL LH YES NO 

## D YES NO YES NO DETAIL RH YES NO 

## D YES NO YES NO DETAIL YES NO 

## E YES NO YES NO DETAIL LH YES NO 

## F YES NO YES NO DETAIL RH YES NO 

## F YES NO YES NO DETAIL LH YES NO 

## G YES NO YES NO DETAIL RH YES NO 

## G YES NO YES NO DETAIL LH YES NO 

## H YES NO YES NO DETAIL RH YES NO 

## H YES NO YES NO DETAIL LH YES NO 

## J YES NO YES NO DETAIL RH YES NO 

## J YES NO YES NO DETAIL LH YES NO 

## K YES NO YES NO DETAIL RH YES NO 

## K YES NO YES NO DETAIL LH YES NO 

## L YES NO YES NO DETAIL RH YES NO 

## L YES NO YES NO DETAIL LH YES NO 

## M YES NO YES NO DETAIL RH YES NO 

## M YES NO YES NO F_SB_534185_5_AAAA_01_00 Figure A-FAAAA - Sheet 01 Inspection Report
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 2 5

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# @A340 SERVICE BULLETIN Appendix 01

**CONF ALL



### A Z190 FR53.9

FR53.2

FR48

FR37 FR39



## A **B**

**C B** 

**C G**  **F H** 

**E**

**D M**  **K G**  **F J**  **H L**  **L J** 
**K**

F_SB_534185_5_AAAA_02_01 

### M **D**

Figure A-FAAAA - Sheet 02 Inspection Report
DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 3 5

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# @A340 SERVICE BULLETIN REPORTING SHEET 

### TITLE: FUSELAGE - CENTER FUSELAGE - INSPECTION OF RODS IN BELLY FAIRING MODIFICATION No.: None Please complete the appropriate item (A or B): A - SB WILL BE embodied YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiment:

B - SB HAS BEEN embodied on aircraft: Operator comments:
From Airline: Name/Title: Signature: Date: If operational documentation is affected (see Paragraph 1.K of this SB): If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either: Modification Operational Impact (MOI), if available YES/NO Or : Intermediate revision YES/NO Important Information: This SB will only be incorporated in your maintenance and operational documentation if this sheet is returned to Airbus and signed by a duly authorised representative. With the next feasible revision, this will result in - Updating of maintenance documentation to show pre and post SB data. - Updating of maintenance and operational documentation to show post SB data after embodiment. If this SB requires previous or simultaneous accomplishment of other SBs, Airbus shall automatically include them in the manual revisions. Refer to SIL 00-037 for detailed information. Please return this completed sheet to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn: SDC32 Technical Data and Documentation Services FAX: (+33) 5 61 93 28 06 e-mail: sb.reporting@airbus.com or via your Resident Customer Support Office. Alternatively, SB lists via letters or fax are also accepted.

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 1 5

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# @A340 SERVICE BULLETIN QUALITY PERCEPTION FORM Use this form to tell us what is your perception of the quality of this Service Bulletin. The reported data that you provide us will be used to analyse areas of difficulties and to take corrective action to further improve the quality of our Service Bulletins. We thank you for the time you have taken in completing this form. (Please rate on a scale of 1 to 4, with 4 being the highest score) - Quality rating of this SB 4 3 2 1 - Quality rating of the Accomplishment Instructions 4 3 2 1 - Quality rating of the Illustrations 4 3 2 1 - Is this SB easy to understand ? Y / N If you have had difficulties in the accomplishment of this SB please quote below the area(s) and give a short description of the issue. Planning Material Instructions X Effectivity X Kit content X Preparation X Reason X List of Materials Operator Supplied X Mod/Inspection X Manpower X Industry support X Test X References X Re-identification X Close-Up X Publication X Tooling X Illustrations Comments:

Operator: Date: Name/Title: Please return this form to: AIRBUS CUSTOMER SERVICES DIRECTORATE 1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.

DATE: Jan 17/11 SERVICE BULLETIN No.: A340-53-4185 REVISION No.: 01 - Apr 07/11 Page: 1 5

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