# @A310 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. 

# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 29 

### TITLE: HYDRAULIC POWER - BRACKETS AND SUPPORTS- HYDRAULIC COMPARTMENT - INSTALL PLACARD FOR HYDRAULIC ACCUMULATOR **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR None MINOR 13540S22823 NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Old generation of hydraulic accumulators (pre 1984) have three welds. They can cause damage on the systems if the accumulators burst. A modification has been developed to change the design from three welds to one weld and to install placard to indicate area where hydraulic accumulators of old generation are forbidden. Installation of accumulator with only one weld (post 1984) will be allowed. This Service Bulletin requires installing : - A support bracket and placard adjacent to the green hydraulic system accumulators Accomplishment of this Service Bulletin will avoid inadvertent installation of (pre 1984) accumulator. 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 DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 1 5

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# @A310 SERVICE BULLETIN SUMMARY EVALUATION TABLE COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED NO NOTE (1): Service Bulletin must be accomplished. MATERIAL PRICE INFORMATION MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Kit 292100A01R00 1 197.00 Support EFFECTIVITY This Service Bulletin is applicable to this (these) operator(s) :

19U 52X 58X 82Z 83V 99Y ACQ AFG AIB AIC BAF BBC BLE CFC CSA DAH DEC DGA F2I FDX G8E GAF HFY I2L IRA IRM IYE JAB JAV K1P KAC KTC KYV KZU MGL MWA PIA QAF R1T RJA ROT RZO SBI SGX SUD THY TSC UZB WHT WTJ CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the simultaneous accomplishment of the following Service Bulletin : A310-29-2099 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 292100-831-801-001: Modification TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 2 5

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# @A310 SERVICE BULLETIN SUMMARY APPENDICES None

DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 3 5

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# @A310 SERVICE BULLETIN SUMMARY

**CONF ALL

FR47 FR54

SUPPORT AND PLACARD Z147

### A
**B**

**C**

SUPPORT AND PLACARD TO

FR52

FR52

**FWD** 

## B **C** 291070 

## A

B_SB_292100_5_SAAA_01_02 TO BE INSTALLED BE INSTALLED

Figure A-FSAAA - Sheet 01

DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 4 5

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# @A310 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



# MANDATORYMANDATORYMANDATORY
ATA SYSTEM: 29 

### TITLE: HYDRAULIC POWER - BRACKETS AND SUPPORTS- HYDRAULIC COMPARTMENT - INSTALL PLACARD FOR HYDRAULIC ACCUMULATOR MODIFICATION No.: 13540S22823 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 NOTE: This modification is applicable by Service Bulletin only. (1) Models 310-203 310-204 310-221 310-222 310-304 310-308 310-322 310-324 310-325 (2) Effectivity by MSN 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0291 0293 0297 0303 0309 0313 0316 0318 0320 0326 0331 0333 0335 0338-0339 0342-0343 0345-0346 0353 0355-0357 0359-0360 0362 0364 0367 0369-0370 0372 0375 0378-0379 0386 0389-0390 0392 0394 0397 0399-0400 0406-0407 0410 0413 0416 0418-0419 0421-0422 0425 0427-0429 0431 0434 0436-0437 0439 0441 0444-0449 0452 0454 0456-0458 0467 0472-0473 0475-0476 0478 0480-0492 0494-0500 0502-0503 0519-0520 0522-0524 0526-0527 0531 0534 0537-0539 0541-0542 0544-0545 0547 0549-0552 0562 0564-0565 0567-0568 0571 0573-0574 0576 0585-0588 0590-0595 0597 0599-0600 0620 0622 0624 0636 0638 0640 0642 0644 0646-0654 0656 0658 0660-0661 0663 DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 1 5

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# @A310 SERVICE BULLETIN

0665 0667 0669 0671-0672 0674 0676 0678 0680 0682 0684 0686-0687 0689 0691 0693 0697 0700 0702 0704 0706 (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 19U 0399 52X 0410 58X 0431 82Z 0550 0551 83V 0427 99Y 0489 ACQ 0538 0544 AFG 0496 0497 AIB 0686 AIC 0392 0406 0407 0413 0428 0429 0654 0665 0669 0680 BAF 0367 0372 BBC 0594 0642 0700 BLE 0650 0674 CFC 0425 0441 0444 0446 0482 CSA 0672 DAH 0291 0293 DEC 0684 0693 0697 DGA 0418 0421 0422 F2I 0309 0487 FDX 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0297 0303 0313 0316 0318 0326 0331 0333 0335 0339 0342 0343 0345 0346 0353 0355 0356 0359 0360 0362 0364 0369 0378 0394 0397 0400 0439 0449 0452 0454 0456 0457 0458 0467 0492 0500 0534 0539 0542 0549 0552 0593 0638 G8E 0475 GAF 0434 0484 0498 0499 0503 0522 0523 HFY 0495 0565 I2L 0640 IRA 0338 0370 0375 0379 0389 0390 0436 0671 IRM 0488 0537 0564 0586 0595 IYE 0568 0702 0704 JAB 0320 0419 JAV 0357 0481 K1P 0648 KAC 0647 0649 0663 KTC 0524 0567 0620 DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 2 5

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# @A310 SERVICE BULLETIN

OPERATOR MSN KYV 0386 KZU 0592 0622 0646 MGL 0526 MWA 0652 PIA 0473 0585 0587 0590 0653 0656 0660 0676 0678 0682 0687 0689 0691 QAF 0667 R1T 0591 RJA 0416 0445 0490 0491 0531 ROT 0636 0644 RZO 0571 0624 0651 0661 SBI 0486 0520 SGX 0519 0562 SUD 0437 THY 0476 0478 0480 0502 TSC 0447 0472 0483 0485 0527 0541 0545 0547 0588 0597 0599 0600 0658 UZB 0574 0576 0706 WHT 0448 0573 WTJ 0494 (4) Configuration by MSN MSN CONFIGURATION 0162 0191 0201 0217 0224 0230 0233 0237 0241 0245 0248 0251 0254 0257 0260 0264 0267 0273 0278 0281 0283 0288 0291 0293 0297 0303 0309 0313 0316 0318 0320 0326 0331 0333 0335 0338 0339 0342 0343 0345 0346 0353 0355 0356 0357 0359 0360 0362 0364 0367 0369 0370 0372 0375 0378 0379 0386 0389 0390 0392 0394 0397 0399 0400 0406 0407 0410 0413 0416 0418 0419 0421 0422 0425 0427 0428 0429 0431 0434 0436 0437 0439 0441 0444 0445 0446 0447 0448 0449 0452 0454 0456 0457 0458 0467 0472 0473 0475 0476 0478 0480 0481 0482 0483 0484 0485 0486 0487 0488 0489 0490 0491 0492 0494 0495 0496 0497 0498 0499 0500 0502 0503 0519 0520 0522 0523 0524 0526 0527 0531 0534 0537 0538 0539 0541 0542 0544 0545 0547 0549 0550 0551 0552 0562 0564 0565 0567 0568 0571 0573 0574 0576 0585 0586 0587 0588 0590 0591 0592 0593 0594 0595 0597 0599 0600 0620 0622 0624 0636 0638 0640 0642 0644 0646 0647 0648 0649 0650 0651 0652 0653 0654 0656 0658 0660 0661 0663 0665 0667 0669 0671 0672 0674 0676 0678 0680 0682 0684 0686 0687 0689 0691 0693 0697 0700 0702 0704 0706 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. DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 3 5

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# @A310 SERVICE BULLETIN (6) Material Effectivity MATERIAL QTY PER A/C SEE NOTES Kit 292100A01R00 1 Consumable CMLA01 1 B. CONCURRENT REQUIREMENTS Accomplishment of this Service Bulletin requires the simultaneous accomplishment of the following Service Bulletin : A310-29-2099 C. REASON (1) History Old generation of hydraulic accumulators (pre 1984) have three welds. They can cause damage on the systems if the accumulators burst. A modification has been developed to change the design from three welds to one weld and to install placard to indicate area where hydraulic accumulators of old generation are forbidden. Installation of accumulator with only one weld (post 1984) will be allowed. (2) Objective/Action This Service Bulletin requires installing : - A support bracket and placard adjacent to the green hydraulic system accumulators (3) Advantages Accomplishment of this Service Bulletin will avoid inadvertent installation of (pre 1984) accumulator. (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : Task 292100-831-801-001: Modification (1) Install the Support and Placard of the Green System Accumulator FIN 291070 E. COMPLIANCE (1) Classification MANDATORY: Service Bulletin must be accomplished. DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 4 5

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# @A310 SERVICE BULLETIN (2) Accomplishment Timescale Accomplishment of this Service Bulletin is requested within 6000 Flight Hours (FH) or 30 months after the issue date of the Service Bulletin whichever occurs first. 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 and/or intervals and/or date) given above but reference should be made to the AD for confirmation of the mandated accomplishment timescale. 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 292100-831-801-001: Modification Get Access 1.00 On Aircraft Install the Support and Placard of the Green System Accumulator FIN 291070 1.00 Close-Up 1.00 TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 H. WEIGHT AND BALANCE Not Changed I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES

Aircraft Maintenance Manual (AMM) 20-21-12 20-28-11 24-00-00 31-12-11 32-12-11 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-51-20 20-55-00 Service Bulletin (SB) A310-29-2099 DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 5 5

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# @A310 SERVICE BULLETIN
Standards Manual (SM) Structural Repair Manual (SRM) 51-23-10 51-24-00 51-40-20 51-40-30 51-40-40 K. PUBLICATION AFFECTED

Aircraft Maintenance Manual (AMM) 29-11-56 Illustrated Parts Catalog (IPC) 53-15-03 L. INTERCHANGEABILITY/MIXABILITY Not Applicable M. SPARES None

DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 6 5

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# @A310 SERVICE BULLETIN
2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Kit 292100A01R00 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 : AIRBUS Material, Logistics and Suppliers Weg beim Jaeger 150 D-22335 Hamburg Germany For ordering by internet : http : //spares.airbus.com For ordering modification kits by fax : +49 40 50 76 25 90 For ordering of single spares by fax : +49 40 50 76 40 13 (2) Price and Availability

Kit 292100A01R Cost 197.00 USD Availability 90 calendar days from receipt of order B. INDUSTRY SUPPORT INFORMATION AIRBUS will provide a 10% reduction to the applicable sales prices given in the paragraph ’Price and Availability’ for orders placed before Dec 31/16. AIRBUS will not provide industry support for accomplishment of this Service Bulletin. C. LIST OF COMPONENTS Kit 292100A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES 1 A2913203300000 1 SUPPORT 2 NAS1801-08-7 2 BOLT 3 NAS1149FN832P 2 WASHER 4 MS21042L08 2 NUT 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.
DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 7 5

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# @A310 SERVICE BULLETIN
D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005E As required Solvent General Purpose 11-026 As required (2) Components None (3) Equipment None E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 8 5

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# @A310 SERVICE BULLETIN
3. ACCOMPLISHMENT INSTRUCTIONS Task 292100-831-801-001 - Modification 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 147 Access Door 734 Manpower TOTAL MANHOURS 3.00 ELAPSED TIME (HOURS) 3.00 A. GENERAL (1) Subtask 292100-839-001-001 - Administrative Manpower Resources Skills NON SPECIFIC (a) Write in the applicable aircraft records that you have done all the work given in this Service Bulletin. (2) Subtask 292100-910-001-001 - Standard Practices Manpower Resources Skills NON SPECIFIC

DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 9 5

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# @A310 SERVICE BULLETIN
Material necessary to do the job Consumable CMLA01 ITEM DESCRIPTION REFERENCE TO CML MAT. No. QTY PER A/C SEE NOTES Interfay Sealant 09-005E As required Solvent General Purpose 11-026 As required References Aircraft Maintenance Manual (AMM) 20-21-12, Page Block 001 20-28-11, Page Block 001 Consumable Material List (CML) Elec. Std. Practices Manual (ESPM) 20-51-20 Structural Repair Manual (SRM) 51-23-10 51-24-00 51-40-20 51-40-30 51-40-40 (a) For the specifications of the materials numbers (Mat.No) (Refer to Consumable Material List (CML)). (b) For the removal and installation of fasteners (Refer to SRM 51-40-20). (c) For alternative and substitute fasteners (Refer to SRM 51-40-30). (d) For fastener hole diameters and drill data (Refer to SRM 51-40-40). (e) To torque tighten the standard threaded fasteners (Refer to AMM 20-21-12, Page Block 001). (f) Use a non-metallic spatule to remove the sealant and clean the areas with : Solvent General Purpose 11-026 As required (g) Apply : Interfay Sealant 09-005E As required to interfaces of structure and new parts, (Refer to SRM 51-24-00). (h) Renew the protective finish, (Refer to SRM 51-23-10). (i) Do the electrical bonding (Refer to ESPM 20-51-20 and AMM 20-28-11, Page Block 001).

DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 10 5

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# @A310 SERVICE BULLETIN
B. PREPARATION (1) Subtask 292100-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 24-00-00, Page Block 301 32-12-11, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put access platform(s) in position. (c) Open the LH main landing gear door 734 (Refer to AMM 32-12-11, Page Block 301). C. PROCEDURE (1) Subtask 292100-420-001-001 - Install the Support and Placard of the Green System Accumulator FIN 291070 Work Zones and Access Panels Zone Access/Work location 147 Access Door 734 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills AIRFRAME Material necessary to do the job Kit 292100A01R00 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES 1 A2913203300000 1 SUPPORT 2 NAS1801-08-7 2 BOLT 3 NAS1149FN832P 2 WASHER 4 MS21042L08 2 NUT References Fig. A-FBAAA Install the Support and Placard of the Green System Accumulator FIN 291070 Sheet 01 Sheet 02 (a) Put the support and placard Item 1 in position as shown in Fig. A-FBAAA Sheet 01 and Fig. A-FBAAA Sheet 02

. DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 11 5

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# @A310 SERVICE BULLETIN (b) Drill two holes on the structure to a diameter between 4.3 mm (0.169 in.) and 4.4 mm (0.173 in.) to match the holes of the support Item 1 as shown in Fig. A-FBAAA Sheet 02

. (c) Install : 1 Support A2913203300000 Item 1 2 Bolt NAS1801-08-7 Item 2 2 Washer NAS1149FN832P Item 3 2 Nut MS21042L08 Item 4 D. TEST None E. CLOSE-UP (1) Subtask 292100-942-001-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 31-12-11, Page Block 301 (a) Make sure that the work areas are clean and clear of tools and other items of equipment (b) Close the LH main landing gear door 734 (Refer to AMM 31-12-11, Page Block 301). (c) Remove the access platform(s). (d) Restore the systems and the aircraft to normal operating conditions.

DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 12 5

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# @A310 SERVICE BULLETIN

**CONF ALL

FR47 FR54



## A Z147

### A
**B**

**C D**  FR52

FR52

**FWD** 

## B **C** 1 291070

B_SB_292100_5_BAAA_01_01 Figure A-FBAAA - Sheet 01 Install the Support and Placard of the Green System Accumulator FIN 291070 DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 13 5

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# @A310 SERVICE BULLETIN

**CONF ALL

5 mm (0.197 in) FR52

1

**FWD**

HOLE SYMBOL ITEM PN DESCRIPTION HOLE DIAMETER MIN MAX
4.30 mm (0.169 in) 4.40 mm (0.173 in) NAS1801−08−7 BOLT NAS1149FN832P WASHER MS21042L08 NUT 2 3 4 B_SB_292100_5_BAAA_02_01 N HEAD ON VISIBLE FACE **NOTE:** DO THE ELECTRICAL BONDING 01 ON BOTH SIDES (AS 2 POINTS). 01

N 

## D

Figure A-FBAAA - Sheet 02 Install the Support and Placard of the Green System Accumulator FIN 291070 DATE: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 14 5

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# @A310 SERVICE BULLETIN REPORTING SHEET 

### TITLE: HYDRAULIC POWER - BRACKETS AND SUPPORTS- HYDRAULIC COMPARTMENT - INSTALL PLACARD FOR HYDRAULIC ACCUMULATOR MODIFICATION No.: 13540S22823 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: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 1 5

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# @A310 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: Aug 12/10 SERVICE BULLETIN No.: A310-29-2100 REVISION No.: 00 - Aug 12/10 Page: 1 5

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