# @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. ATA SYSTEM: 22 

### TITLE: AUTO FLIGHT - FCC - INSTALL FCC PN B470ADM3 CAPABLE OF RUDDER REVERSAL WARNING **CONF ALL MODIFICATIONS MODIFICATION CLASSIFICATION MAJOR 13591S22844 MINOR None NOTE: As per EASA IR 21, a minor change is one that has no appreciable effect on the mass, balance, structural strength, reliability, operational characteristics affecting the airworthiness of the product. All other changes are major changes. REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Following report of events of rapid alternating and large rudder pedal inputs that resulted in high vertical stabilizer loads, a new function has been developed in the Flight Control Computer (FCC) to detect excessive pedal reversal inputs in order to trigger visual and aural warnings via Flight Warning Computer (FWC). This Service Bulletin is published to advise all operator of A310 aircraft of the issue of THALES AVIONICS S.A. Service Bulletin No. B470ADM-22-006. This Service Bulletin upgrades: - the two FCCs PN B470ADM by the new ones FCCs PN B470ADM3 capable of rudder reversal warning modified as per instructions given in the THALES AVIONICS S.A. Service Bulletin No. B470ADM-22-006. Or replaces: - the two FCCs PN B350AAM6 by the new ones FCCs PN B470ADM3. When Service Bulletin No. A310-22-2063, Service Bulletin No. A310-22-2064, Service Bulletin No. A310-22-2065 and Service Bulletin No. A310-31-2144 are embodied, in case of excessive rudder pedal reversal inputs, visual and aural warnings are triggered in the cockpit: - The FWC provides audio "STOP RUDDER INPUT" messages.
DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 1 5

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# @A310 SERVICE BULLETIN SUMMARY - STOP rudder inputs lights are illuminated. GENERAL EVALUATION EVALUATION TABLE COMPLIANCE RECOMMENDED (1) CANCELS INSPECTION SB NO POTENTIAL AD YES A/C OPERATION AFFECTED NO RELIABILITY AFFECTED NO PAX COMFORT AFFECTED NO COST SAVING NO ETOPS AFFECTED NO STRUCTURAL LIFE EXTN NO VENDOR SB INVOLVED YES NOTE (1): Service Bulletin recommended to be accomplished to prevent significant operational disruptions. MATERIAL PRICE INFORMATION **CONF 001 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Equipment BFEA01 1 See SB FCCs **CONF 002 MATERIAL PRICE INFORMATION TABLE MATERIAL SET QTY PER A/C PRICE PER A/C (USD) MAIN PARTS Equipment BFEA02 1 See SB FCCs EFFECTIVITY **CONF ALL This Service Bulletin is applicable to this (these) operator(s) :

18T 19U 52X 58X 82Z 83V 85W 85Z 99Y AFG AIB AIC AMV BAF BBC C9L CFC DAH DGA FDX G2X G8E GAF HFY HJI IRA IRM IYE JAV K1P KAC KZU MGL PCA PIA QAF R1T RJA ROT RZO SBI SGX THY TSC UBD UZB WHT CONCURRENT REQUIREMENTS **CONF 001 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletins or the equivalent production modifications:

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 2 5

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# @A310 SERVICE BULLETIN SUMMARY Service Bulletin No. A310-22-2049 Mod. No. 11900S21544 11900S21561 11900S21601 11900S21602 11900S21628 A310-22-2062 10402S20536 10402S20624 11900S21544 11900S21561 11900S21601 11900S21602 11900S21628 12041S21720 13389S29069 NOTE: Accomplish either Service Bulletin No. A310-22-2049 or Service Bulletin No. A310-22-2062 as per effectivity specified in these Service Bulletins. **CONF 002 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin or the equivalent production modification: Service Bulletin No. A310-22-2048 Mod. No. 11899S21543 11899S21560 11899S21627 REFERENCES / REPERCUSSIONS **CONF ALL TFU None OEB None AOT None SIL None LINE MAINTENANCE AFFECTED No LIFE LIMIT None OTHER None NATURE OF THE WORK AIRCRAFT NO EQUIPMENT YES HARD NO SOFT YES OBRM NO

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 3 5

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# @A310 SERVICE BULLETIN SUMMARY MANPOWER **CONF 001 Task 222065-831-801-001: Modification of the two FCCs by replacement or by reprogramming of their cards. TOTAL MANHOURS 5.00 ELAPSED TIME (HOURS) 5.00 Additional manhours related to Vendor SB; refer to: Modify the two FCCs (FINs 301CA1 and 301CA2). THALES AVIONICS S.A. Service Bulletin No. B470ADM-22-006 Task 222065-831-802-001: Modification by replacement of the two FCCs. TOTAL MANHOURS 5.00 ELAPSED TIME (HOURS) 5.00 **CONF 002 Task 222065-831-802-001: Modification by replacement of the two FCCs. TOTAL MANHOURS 5.00 ELAPSED TIME (HOURS) 5.00 APPENDICES **CONF ALL None

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 4 5

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# @A310 SERVICE BULLETIN SUMMARY

**CONF ALL

FR17 FR20

121BL

80VU LH ELECTRONICS RACK FCC1

FCC2 

### A



## A 301CA1

301CA2

B_SB_222065_5_SAAA_01_01 Figure A-FSAAA - Sheet 01

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 5 5

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# @A310 SERVICE BULLETIN SUMMARY

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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 ATA SYSTEM: 22 

### TITLE: AUTO FLIGHT - FCC - INSTALL FCC PN B470ADM3 CAPABLE OF RUDDER REVERSAL WARNING MODIFICATION No.: 13591S22844 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 0313 0316 0318 0326 0331 0333 0335 0338-0339 0342-0343 0345-0346 0353 0355-0357 0359-0360 0362 0364 0367 0369-0370 0372 0375 0378-0379 0389-0390 0392 0394 0397 0399-0400 0406-0407 0410 0413 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 0480-0485 0488-0492 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 0642 0644 0646-0654 0656 0658 0660-0661 0663 0667 0669 0671-0672 0674 0676 0678 0682 0684 0686-0687 0689 0691 0693 0697 0700 0702 0704 0706

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# @A310 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 18T 0473 19U 0399 52X 0410 58X 0431 82Z 0550 0551 83V 0427 85W 0684 0693 0697 85Z 0547 99Y 0489 AFG 0496 0497 AIB 0650 0686 AIC 0392 0406 0407 0428 0429 0538 0544 0654 0669 AMV 0437 BAF 0367 0372 BBC 0594 0642 0700 C9L 0652 CFC 0425 0441 0444 0446 0482 DAH 0291 0293 DGA 0418 0421 0422 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 G2X 0573 G8E 0475 GAF 0434 0484 0498 0499 0503 0522 0523 HFY 0495 0565 HJI 0413 IRA 0338 0370 0375 0379 0389 0390 0436 0671 IRM 0488 0524 0537 0564 0567 0586 0595 0620 IYE 0568 0702 0704 JAV 0357 0481 K1P 0648 KAC 0647 0649 0663 KZU 0592 0622 0646 MGL 0526 PCA 0419 PIA 0585 0587 0590 0653 0656 0660 0676 0678 0682 0687 0689 0691 DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 2 5

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# @A310 SERVICE BULLETIN

OPERATOR MSN QAF 0667 R1T 0591 RJA 0445 0490 0491 0531 ROT 0636 0644 RZO 0571 0624 0651 0661 SBI 0520 SGX 0519 0562 THY 0476 0478 0480 0502 TSC 0447 0472 0483 0485 0527 0541 0545 0588 0597 0599 0600 0658 UBD 0672 0674 UZB 0574 0576 0706 WHT 0448 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 0313 0316 0318 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 0389 0390 0392 0394 0397 0399 0400 0406 0407 0410 0413 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 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 0642 0644 0646 0647 0648 0649 0650 0651 0652 0653 0654 0656 0658 0660 0661 0663 0667 0669 0671 0672 0674 0676 0678 0682 0684 0686 0687 0689 0691 0693 0697 0700 0702 0704 0706 001 002

(5) Configuration definition **CONF 001 Config. 001 is valid for aircraft on which Service Bulletin No. A310-22-2048 is not embodied, Service Bulletin No. A310-22-2249 or Service Bulletin No. A310-22-2062 is embodied and on which PN B470ADM is installed. **CONF 002 Config. 002 is valid for aircraft on which Service Bulletin No. A310-22-2249 or Service Bulletin No. A310-22-2062 is not embodied, Service Bulletin No. A310-22-2048 is embodied and on which PN B350AAM6 is installed.

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 3 5

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# @A310 SERVICE BULLETIN (6) Material Effectivity **CONF 001 MATERIAL QTY PER A/C SEE NOTES Equipment BFEA01 1 **CONF 002 MATERIAL QTY PER A/C SEE NOTES Equipment BFEA02 1 **CONF ALL B. CONCURRENT REQUIREMENTS **CONF 001 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletins or the equivalent production modifications: Service Bulletin No. A310-22-2049 Mod. No. 11900S21544 11900S21561 11900S21601 11900S21602 11900S21628 A310-22-2062 10402S20536 10402S20624 11900S21544 11900S21561 11900S21601 11900S21602 11900S21628 12041S21720 13389S29069 NOTE: Accomplish either Service Bulletin No. A310-22-2049 or Service Bulletin No. A310-22-2062 as per effectivity specified in these Service Bulletins. **CONF 002 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin or the equivalent production modification: Service Bulletin No. A310-22-2048 Mod. No. 11899S21543 11899S21560 11899S21627

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 4 5

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# @A310 SERVICE BULLETIN

**CONF ALL C. REASON (1) History Following report of events of rapid alternating and large rudder pedal inputs that resulted in high vertical stabilizer loads, a new function has been developed in the Flight Control Computer (FCC) to detect excessive pedal reversal inputs in order to trigger visual and aural warnings via Flight Warning Computer (FWC). (2) Objective/Action This Service Bulletin is published to advise all operator of A310 aircraft of the issue of THALES AVIONICS S.A. Service Bulletin No. B470ADM-22-006. This Service Bulletin upgrades: - the two FCCs PN B470ADM by the new ones FCCs PN B470ADM3 capable of rudder reversal warning modified as per instructions given in the THALES AVIONICS S.A. Service Bulletin No. B470ADM-22-006. Or replaces: - the two FCCs PN B350AAM6 by the new ones FCCs PN B470ADM3. (3) Advantages When Service Bulletin No. A310-22-2063, Service Bulletin No. A310-22-2064, Service Bulletin No. A310-22-2065 and Service Bulletin No. A310-31-2144 are embodied, in case of excessive rudder pedal reversal inputs, visual and aural warnings are triggered in the cockpit: - The FWC provides audio "STOP RUDDER INPUT" messages. - STOP rudder inputs lights are illuminated. (4) Operational/Maintenance Consequences None D. DESCRIPTION NOTE: To accomplish this Service Bulletin, you have two possibilities: - either you modify the two FCCs by replacement or by reprogramming their cards as described in TASK 222065-831-801 001 Modification of the two FCCs by replacement or by reprogramming of their cards. - or you replace them as described in TASK 222065-831-802 001 Modification by replacement of the two FCCs. To accomplish this Service Bulletin it is necessary to : DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 5 5

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# @A310 SERVICE BULLETIN

**CONF 001 Task 222065-831-801-001: Modification of the two FCCs by replacement or by reprogramming of their cards. (1) In the LH electronics rack 80VU, remove the two FCCs (FINs 301CA1 and 301CA2). (2) Modify the two FCCs (FINs 301CA1 and 301CA2). (3) In the LH electronics rack 80VU, install the two FCCs (FINs 301CA1 and 301CA2). Task 222065-831-802-001: Modification by replacement of the two FCCs. (1) In the LH electronics rack 80VU, replace the two FCCs (FINs 301CA1 and 301CA2). **CONF 002 Task 222065-831-802-001: Modification by replacement of the two FCCs. (1) In the LH electronics rack 80VU, replace the two FCCs (FINs 301CA1 and 301CA2). **CONF ALL E. COMPLIANCE (1) Classification RECOMMENDED: Service Bulletin recommended to be accomplished to prevent significant operational disruptions. (2) Accomplishment Timescale Accomplishment of this Service Bulletin is recommended at the earliest opportunity where manpower and facilities are available. F. APPROVAL The technical content of this document is approved under the authority of Design Organization 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. DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 6 5

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# @A310 SERVICE BULLETIN

**CONF 001 Task 222065-831-801-001: Modification of the two FCCs by replacement or by reprogramming of their cards. Get Access 1.00 On Aircraft In the LH electronics rack 80VU, remove the two FCCs (FINs 301CA1 and 301CA2). 1.00 In the LH electronics rack 80VU, install the two FCCs (FINs 301CA1 and 301CA2). 1.00 Tests 1.00 Close-Up 1.00 TOTAL MANHOURS 5.00 ELAPSED TIME (HOURS) 5.00 Additional manhours related to Vendor SB; refer to: Modify the two FCCs (FINs 301CA1 and 301CA2). THALES AVIONICS S.A. Service Bulletin No. B470ADM-22-006 Task 222065-831-802-001: Modification by replacement of the two FCCs. Get Access 1.00 On Aircraft In the LH electronics rack 80VU, replace the two FCCs (FINs 301CA1 and 301CA2). 2.00 Tests 1.00 Close-Up 1.00 TOTAL MANHOURS 5.00 ELAPSED TIME (HOURS) 5.00 **CONF 002 Task 222065-831-802-001: Modification by replacement of the two FCCs. Get Access 1.00 On Aircraft In the LH electronics rack 80VU, replace the two FCCs (FINs 301CA1 and 301CA2). 2.00 Tests 1.00 Close-Up 1.00 TOTAL MANHOURS 5.00 ELAPSED TIME (HOURS) 5.00 **CONF ALL H. WEIGHT AND BALANCE Not Changed

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 7 5

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# @A310 SERVICE BULLETIN

I. ELECTRICAL LOAD DATA Not Changed J. REFERENCES **CONF 001 Aircraft Maintenance Manual (AMM) 22-18-34 24-00-00 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A310-22-2049 A310-22-2062 A310-22-2063 A310-22-2064 A310-22-2065 A310-31-2144 Vendor Service Bulletin (VSB) THALES AVIONICS S.A. Service Bulletin No. B470ADM-22-006 **CONF 002 Aircraft Maintenance Manual (AMM) 22-18-34 24-00-00 ATA Common Support Data Dictionary (CSDD), Chapter 2 Elec. Std. Practices Manual (ESPM) 20-55-00 Service Bulletin (SB) A310-22-2048 A310-22-2063 A310-22-2064 A310-22-2065 A310-31-2144 **CONF ALL K. PUBLICATION AFFECTED

Illustrated Parts Catalog (IPC) 22-18-08 L. INTERCHANGEABILITY/MIXABILITY **CONF 001 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES FCC B470ADM B470ADM3 03 NO (1) NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved.
DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 8 5

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# @A310 SERVICE BULLETIN

NOTE (1): Mixability not authorized. Replacement of the two FCCs has to be done simultaneously as per ACCOMPLISHMENT INSTRUCTIONS paragraph 3.C of this Service Bulletin. **CONF 002 DESCRIPTION OLD PART N ̊ NEW PART N ̊ INT MIXABILITY SEE NOTES FCC B350AAM6 B470ADM3 03 NO (1) NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE: Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved. NOTE (1): Mixability not authorized. Replacement of the two FCCs has to be done simultaneously as per ACCOMPLISHMENT INSTRUCTIONS paragraph 3.C of this Service Bulletin. **CONF ALL M. SPARES FCC B350AAM6 FCC B470ADM

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 9 5

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# @A310 SERVICE BULLETIN

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# @A310 SERVICE BULLETIN

2. MATERIAL INFORMATION **CONF ALL A. MATERIAL - PRICE AND AVAILABILITY (1) Procurement Addresses Equipment BFEA01 Equipment BFEA02 The material is included in the commercial offer of the Letter Agreement, and as such will be supplied by AIRBUS Upgrade Services. Airline Customers are requested to contact: AIRBUS Upgrade Services Attn KAM Manager (2) Price and Availability Sales terms must be agreed between the Customer and AIRBUS in accordance with the RFC (or RFC/RMO) procedure in the framework of the Stop Rudder Inputs Warning retrofit. B. INDUSTRY SUPPORT INFORMATION Refer to the paragraph: ’Price and Availability’. C. LIST OF COMPONENTS No Kit D. LIST OF MATERIALS - OPERATOR SUPPLIED (1) Consumable Materials None (2) Components None (3) Equipment Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES B470ADM3 2 FCC B470ADM 03 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2.
DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 11 5

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# @A310 SERVICE BULLETIN Equipment BFEA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD ITEM OLD PART N ̊ INT SEE NOTES B470ADM3 2 FCC B350AAM6 03 NOTE: For definitions of interchangeability codes in column INT., refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. E. PARTS TO BE RE-IDENTIFIED BY OPERATOR None F. TOOLING None

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 12 5

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# @A310 SERVICE BULLETIN

3. ACCOMPLISHMENT INSTRUCTIONS Task 222065-831-801-001 - Modification of the two FCCs by replacement or by reprogramming of their cards. 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. NOTE: This Task concerns the modification of the FCCs by replacement or by reprogramming their cards. Task Associated Data **CONF 001 Zone 120 Modified FIN 301CA1 301CA2 Manpower TOTAL MANHOURS 5.00 ELAPSED TIME (HOURS) 5.00 Additional manhours related to Vendor SB; refer to: THALES AVIONICS S.A. Service Bulletin No. B470ADM-22-006 **CONF 002 None

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# @A310 SERVICE BULLETIN

**CONF ALL A. GENERAL **CONF 001 (1) Subtask 222065-839-001-001 - 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. **CONF 002 None **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 222065-941-001-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401 24-00-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put the access platform in position below the door 121BL and the door 831 or 841. (c) Open the door 121BL and the door 831 or 841. (d) Do the Job Set-Up as specified in the removal/installation of the FCCs (FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401). **CONF 002 None

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# @A310 SERVICE BULLETIN

**CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 222065-020-001-001 - In the LH electronics rack 80VU, remove the two FCCs (FINs 301CA1 and 301CA2). Work Zones and Access Panels Zone Access/Work location 120 Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401 (a) Remove the two FCCs (FINs 301CA1 and 301CA2): Refer to AMM 22-18-34, Page Block 401 FIN 301CA1 1 FCC B470ADM and FIN 301CA2 1 FCC B470ADM

(2) Subtask 222065-831-001-001 - Modify the two FCCs (FINs 301CA1 and 301CA2). References Vendor Service Bulletin (VSB) THALES AVIONICS S.A. B470ADM-22-006 (a) Modify the two FCCs (FINs 301CA1 and 301CA2) (Refer to THALES AVIONICS S.A. Service Bulletin No. B470ADM-22-006). (3) Subtask 222065-420-001-001 - In the LH electronics rack 80VU, install the two FCCs (FINs 301CA1 and 301CA2). Work Zones and Access Panels Zone Access/Work location 120

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 15 5

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# @A310 SERVICE BULLETIN
Manpower Resources Manhours 1.00 Minimum number of person 1 Subtask elapsed time 1.00 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES B470ADM3 2 FCC References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401 (a) Install the two FCCs (FINs 301CA1 and 301CA2): Refer to AMM 22-18-34, Page Block 401 FIN 301CA1 1 FCC B470ADM3 and FIN 301CA2 1 FCC B470ADM3 **CONF 002 None **CONF ALL D. TEST **CONF 001 (1) Subtask 222065-700-001-001 - Test Work Zones and Access Panels Zone Access/Work location 120 Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 16 5

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# @A310 SERVICE BULLETIN (a) Job Set-Up: 1 Remove the safety clips and/or tags and close/unlock the circuit breakers as specified after the installation of the FCCs (FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401). (b) Procedure: 1 Do the test procedure as specified after the installation of the FCCs (FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401). **CONF 002 None **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 222065-942-001-001 - Close-up Work Zones and Access Panels Zone Access/Work location 120 Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the Close-up procedure as specified in the removal/installation of the FCCs (FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401). (c) Close the access doors. (d) Remove the access platform(s). (e) Restore the systems and the aircraft to the normal operating condition. **CONF 002 None

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 17 5

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# @A310 SERVICE BULLETIN

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DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 18 5

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# @A310 SERVICE BULLETIN Task 222065-831-802-001 - Modification by replacement of the two FCCs. **CONF ALL 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. NOTE: This Task concerns the replacement of the two FCCs. Task Associated Data **CONF 001 Zone 120 Modified FIN 301CA1 301CA2 Manpower TOTAL MANHOURS 5.00 ELAPSED TIME (HOURS) 5.00 **CONF 002 Zone 120 Modified FIN 301CA1 301CA2 Manpower TOTAL MANHOURS 5.00 ELAPSED TIME (HOURS) 5.00

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 19 5

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# @A310 SERVICE BULLETIN

**CONF ALL A. GENERAL **CONF 001 (1) Subtask 222065-839-002-001 - 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. **CONF 002 (1) Subtask 222065-839-002-002 - 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. **CONF ALL B. PREPARATION **CONF 001 (1) Subtask 222065-941-002-001 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401 24-00-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put the access platform in position below the door 121BL and the door 831 or 841. (c) Open the door 121BL and the door 831 or 841. (d) Do the Job Set-Up as specified in the removal/installation of the FCCs (FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401).

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 20 5

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# @A310 SERVICE BULLETIN

**CONF 002 (1) Subtask 222065-941-002-002 - Job Set-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401 24-00-00, Page Block 301 (a) Make sure that the aircraft is electrically grounded (Refer to AMM 24-00-00, Page Block 301). (b) Put the access platform in position below the door 121BL and the door 831 or 841. (c) Open the door 121BL and the door 831 or 841. (d) Do the Job Set-Up as specified in the removal/installation of the FCCs (FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401). **CONF ALL C. PROCEDURE **CONF 001 (1) Subtask 222065-960-001-001 - In the LH electronics rack 80VU, replace the two FCCs (FINs 301CA1 and 301CA2). Work Zones and Access Panels Zone Access/Work location 120 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA01 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES B470ADM3 2 FCC References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 21 5

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# @A310 SERVICE BULLETIN (a) Remove the two FCCs (FINs 301CA1 and 301CA2): Refer to AMM 22-18-34, Page Block 401 FIN 301CA1 1 FCC B470ADM and FIN 301CA2 1 FCC B470ADM (b) Install the two FCCs (FINs 301CA1 and 301CA2): Refer to AMM 22-18-34, Page Block 401 FIN 301CA1 1 FCC B470ADM3 and FIN 301CA2 1 FCC B470ADM3 **CONF 002 (1) Subtask 222065-960-001-002 - In the LH electronics rack 80VU, replace the two FCCs (FINs 301CA1 and 301CA2). Work Zones and Access Panels Zone Access/Work location 120 Manpower Resources Manhours 2.00 Minimum number of person 1 Subtask elapsed time 2.00 Skills NON SPECIFIC Material necessary to do the job Equipment BFEA02 ITEM NEW PART N ̊ QTY (UM) KEYWORD SEE NOTES B470ADM3 2 FCC References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401 (a) Remove the two FCCs (FINs 301CA1 and 301CA2): Refer to AMM 22-18-34, Page Block 401 DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 22 5

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# @A310 SERVICE BULLETIN

FIN 301CA1 1 FCC B350AAM6 and FIN 301CA2 1 FCC B350AAM6 (b) Install the two FCCs (FINs 301CA1 and 301CA2): Refer to AMM 22-18-34, Page Block 401 FIN 301CA1 1 FCC B470ADM3 and FIN 301CA2 1 FCC B470ADM3 **CONF ALL D. TEST **CONF 001 (1) Subtask 222065-700-002-001 - Test Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401 (a) Job Set-Up: 1 Remove the safety clips and/or tags and close/unlock the circuit breakers as specified after the installation of the FCCs (FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401). (b) Procedure: 1 Do the test procedure as specified after the installation of the FCCs (FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401). **CONF 002 (1) Subtask 222065-700-002-002 - Test Manpower Resources Skills NON SPECIFIC

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 23 5

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# @A310 SERVICE BULLETIN

References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401 (a) Job Set-Up: 1 Remove the safety clips and/or tags and close/unlock the circuit breakers as specified after the installation of the FCCs (FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401). (b) Procedure: 1 Do the test procedure as specified after the installation of the FCCs (FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401). **CONF ALL E. CLOSE-UP **CONF 001 (1) Subtask 222065-942-002-001 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Do the Close-up procedure as specified in the removal/installation of the FCCs (FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401). (c) Close the access doors. (d) Remove the access platform(s). (e) Restore the systems and the aircraft to the normal operating condition. **CONF 002 (1) Subtask 222065-942-002-002 - Close-up Manpower Resources Skills NON SPECIFIC References Aircraft Maintenance Manual (AMM) 22-18-34, Page Block 401 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 24 5

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# @A310 SERVICE BULLETIN (b) Do the Close-up procedure as specified in the removal/installation of the FCCs (FINs 301CA1 and 301CA2) (Refer to AMM 22-18-34, Page Block 401). (c) Close the access doors. (d) Remove the access platform(s). (e) Restore the systems and the aircraft to the normal operating condition.

DATE: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 25 5

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# @A310 SERVICE BULLETIN REPORTING SHEET 

### TITLE: AUTO FLIGHT - FCC - INSTALL FCC PN B470ADM3 CAPABLE OF RUDDER REVERSAL WARNING MODIFICATION No.: 13591S22844 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: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 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 4321 - Quality rating of the Accomplishment Instructions 4321 - Quality rating of the Illustrations 4321 - 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: Apr 25/12 SERVICE BULLETIN No.: A310-22-2065 REVISION No.: 00 - Apr 25/12 Page: 1 5

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