# @ A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET

5 DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : 1 of 2 Printed in FRANCE © AIRBUS, 2006 All rights reserved 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 : 27 TITLE : FLIGHT CONTROLS - ELEVATOR AND HYDRAULIC ACTUATION - INTRODUCE NEW SOLENOID VALVE SEALS ON A330/A340 SERVOCONTROLS. MODIFICATION No. : 53969S18340 53976S18343 53977S18344 53978S18345 This page transmits Revision No. 01 of Service Bulletin No. A330-27-3134. ADDITIONAL WORK No additional work is required by this revision for aircraft modified by any previous issue. REASON Revision No. 01 issued to add aircraft MSN 0708 for operator AAR and MSN 0709 for operator MSR. CHANGES SUMMARY : — REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES . Text modified. — EFFECTIVITY . Operators updated. Sentence updated. — MANPOWER . 7.0 hours become 8.0 hours for the TOTAL MANHOURS. 7.0 hours become 8.0 hours for the ELAPSED TIME hours. PLANNING INFORMATION : — EFFECTIVITY . Para. 1.A. Aircraft MSN 0708 added for operator AAR. Aircraft MSN 0709 added for operator MSR. Effectivity updated. NOTE updated. — REASON . Para. 1.C. Text modified.

# @ A330 SERVICE BULLETIN REVISION TRANSMITTAL SHEET

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved — MANPOWER . Para. 1.G. 7.0 hours become 8.0 hours for TOTAL MANHOURS. 7.0 hours become 8.0 hours for ELAPSED TIME hours. 1.0 hour becomes 2.0 hours for the test. — REFERENCES . Para. 1.J. Reference to AD F-2004-158 added. ACCOMPLISHMENT INSTRUCTIONS : — GENERAL . Para. 3.A. Preparation procedure modified. — TESTS . Para. 3.C. Test procedure modified. — CLOSE-UP . Para. 3.D. Close-up procedure modified. NOTE : Layout changes due to computerization of this revision are not identified. FILING 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 revisions. REVISION SEQUENCE ORIGINAL : Oct 13/05 REVISION No. : 01 — May 12/06

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# @ A330 SERVICE BULLETIN SUMMARY

5 DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : 1 of 3 Printed in FRANCE © AIRBUS, 2006 All rights reserved 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 : 27 TITLE : FLIGHT CONTROLS - ELEVATOR AND HYDRAULIC ACTUATION - INTRODUCE NEW SOLENOID VALVE SEALS ON A330/A340 SERVOCONTROLS. MODIFICATION No. : 53969S18340 53976S18343 53977S18344 53978S18345 REASON/DESCRIPTION/OPERATIONAL CONSEQUENCES Further to some reported cases of extrusion and damage of the solenoid valves external preformed packings, a new elevator servocontrol with new capped seals standard has been developed. This Service Bulletin is published to advise all operators of A330 aircraft of the issue of GOODRICH Service Bulletin No. SC4800-27-17. This Service Bulletin recommends modifying the affected servocontrols : — P/N SC4800-72 modified into P/N SC4800-73, — P/N SC4800-92 modified into P/N SC4800-93, — P/N SC4800-10 modified into P/N SC4800-103, — P/N SC4800-11 modified into P/N SC4800-113. Accomplishment of this Service Bulletin will reinforce the pressure fatigue strength of external packings of the solenoid valves and cancels the action introduced by the paragraph 3.1 of the Airworthiness Directive (AD) F-2004-158.

EVALUATION TABLE COMPLIANCE Recommended CANCELS INSPECTION SB No POTENTIAL AD No 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 KIT PRICE (USD) No Kit

# @ A330 SERVICE BULLETIN SUMMARY

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved 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. EFFECTIVITY This Service Bulletin is applicable to these operators : 79X AAR ACA ACI AFR ALK AUA BMA CAL CPA CRL CSN CYP DAH DAT DLH DRD EDW EEZ EIN ETD EVA FWI GFA GIA GRL HDA IWD IYE KAL KLM LTU LVG LXR MAS MEA MON MSR MYT NVR NWA PAL QAF QFA QTR SAS SEU SWR TAM TAP TCX THA THY TSC UAE USA VKG The modification No. 53969S18340 is embodied before delivery on A330 aircraft MSN 0711 and subsequent. The modifications No. 53976S18343, 53977S18344 and 53978S18345 are applicable by Service Bulletin only. CONCURRENT REQUIREMENTS If elevator servocontrols PN SC4800-9 are installed on aircraft : accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin or the equivalent production modification: Service Bulletin No. A330-27-3128 Mod. No. 52947S18075 If elevator servocontrols PN SC4800-7A are installed on aircraft : accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin or the equivalent production modification: Service Bulletin No. A330-27-3128 Mod. No. 53386S18200 REFERENCES/REPERCUSSIONS TFU : 27.34.00.010 OEB : 50, 54 AOT : None SIL : None LIFE LIMIT : None LINE MAINTENANCE AFFECTED : No OTHERS : AD F-2004-158 MODIFICATION CLASSIFICATION MAJOR 53969S18340 53976S18343 53977S18344 53978S18345 MINOR None

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# @ A330 SERVICE BULLETIN SUMMARY

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved NATURE OF THE WORK AIRCRAFT : NO EQUIPMENT : YES HARD : NO SOFT : NO OBRM : NO MANPOWER Config. 01 , on aircraft, modification of the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2

Config. 01 , on aircraft, replacement of the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2

Config. 01 , on bench

MATERIAL INFORMATION AIRCRAFT DATA None APPENDICES None TOTAL MANHOURS 6.5 ELAPSED TIME (HOURS) 6.5

TOTAL MANHOURS 8.0 ELAPSED TIME (HOURS) 8.0

TOTAL MANHOURS Refer to GOODRICH Service Bulletin No. SC4800-27-17 ELAPSED TIME (HOURS) Refer to GOODRICH Service Bulletin No. SC4800-27-17

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# @ A330 SERVICE BULLETIN

5 DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : 1 of 14 Printed in FRANCE © AIRBUS, 2006 All rights reserved 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 : 27 TITLE : FLIGHT CONTROLS - ELEVATOR AND HYDRAULIC ACTUATION - INTRODUCE NEW SOLENOID VALVE SEALS ON A330/A340 SERVOCONTROLS. MODIFICATION No. : 53969S18340 53976S18343 53977S18344 53978S18345 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 A. EFFECTIVITY (1) Models 330-201 330-202 330-203 330-223 330-243 330-301 330-302 330-303 330-321 330-322 330-323 330-341 330-342 330-343 (2) Aircraft (a) Effectivity by MSN This Service Bulletin is applicable to aircraft MSN : 0012 0017 0030 0037 0045 0050 0054 0055 0059 0060 0062 0064-0067 0069-0073 0077 0082 0083 0086 0087 0095 0096 0098-0100 0102 0106 0107 0109-0113 0116 0118-0122 0127 0132 0138 0140 0143 0144 0148 0153 0155 0162 0165 0171 0172 0177 0181 0183 0184 0188 0189 0191 0195 0198 0200 0203 0205 0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238 0240 0241 0244 0247-0251 0253-0256 0258 0259 0261 0262 0265-0267 0269 0271 0272 0275-0277 0279 0281 0283-0288 0290 0291 0293-0296 0299-0301 0303 0305 0306 0308 0309 0311-0317 0320 0322-0324 0326 0328 0330 0333 0334 0337-0340 0342-0346 0348-0351 0353 0356-0358 0361 0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386 0388 0389 0392 0393 0396-0398 0400 0401 0403-0405 0407-0409 0412 0418-0423 0425 0427 0428 0432 0437 0439 0441 0443 0444 0448 0451 0452 0454-0456 0458 0461-0463 0465 0466

# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved 0469 0472 0473 0476 0477 0479-0481 0484 0486 0487 0489-0491 0493 0494 0496-0498 0500-0513 0515 0516 0518 0519 0521 0522 0524-0527 0529 0530 0532 0533 0535 0536 0539 0542 0548-0553 0555 0558 0564 0565 0567 0568 0570 0571 0573 0574 0576 0578 0579 0581 0584 0587 0588 0591 0593 0595 0597 0600 0602 0603 0605 0607 0609 0610 0612 0614 0616 0618 0620 0621 0623 0625 0627 0629 0631-0638 0640-0642 0644 0645 0647-0650 0652-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688 0690-0693 0695-0697 0699-0701 0703-0705 0707-0709 NOTE : The modification No. 53969S18340 is embodied before delivery on A330 aircraft MSN 0711 and subsequent. NOTE (01) The modifications No. 53976S18343, 53977S18344 and 53978S18345 are applicable by Service Bulletin only. (b) 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 79X 0305 0312 AAR 0640 0676 0708 ACA 0277 0279 0284 0344 0400 0408 0412 0419 ACI 0507 0510 AFR 0422 0443 0448 0458 0465 0481 0498 0500 0502 0503 0516 0519 0567 0584 0657 0660 ALK 0303 0306 0311 0313 AUA 0181 0195 0223 0317 BMA 0398 0401 0404 CAL 0602 0607 0641 0671 0675 0691 0699 0707 CPA 0012 0017 0071 0083 0099 0102 0109 0113 0118 0121 0155 0244 0386 0389 0393 0418 0420 0421 0423 0439 0539 0548 0565 0669 0673 0679 CRL 0285 0320 CSN 0649 0652 0656 0664 CYP 0505 0526 DAH 0644 0647 0650 0653 0667 DAT 0030 0037 0045 DLH 0322 0324 0570 0576 0579 0629 0636 0642 0645 0648 0687 0701 DRD 0054 0205 0211 0362

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# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved EDW 0369 EEZ 0358 0364 0665 EIN 0055 0059 0070 0086 0269 0330 0397 ETD 0232 0259 0272 0339 0361 0658 0688 EVA 0530 0535 0555 0573 0587 0634 0655 0661 0678 0693 FWI 0240 0253 GFA 0276 0281 0286 0287 0334 0340 GIA 0138 0140 0144 0148 0153 0165 GRL 0230 HDA 0098 0106 0132 0177 0234 0405 0407 0479 0512 0581 0654 0662 0692 IWD 0072 0461 0670 IYE 0625 0632 KAL 0162 0172 0206 0219 0222 0226 0241 0256 0258 0267 0338 0350 0351 0368 0425 0428 0484 0490 0550 KLM 0682 0686 0703 LTU 0082 0120 0127 0171 0403 0432 0444 0454 0469 0476 0493 LVG 0551 0597 0627 LXR 0087 0096 MAS 0067 0069 0073 0077 0095 0100 0107 0110 0116 0119 0143 0255 0262 0290 0296 0300 MEA 0527 0529 0532 MON 0261 0265 MSR 0600 0610 0666 0683 0696 0709 MYT 0254 0266 0301 NVR 0353 NWA 0524 0533 0542 0549 0552 0578 0588 0591 0609 0614 0618 0620 0621 0631 0633 0663 0674 0690 PAL 0183 0184 0188 0189 0191 0198 0200 0203 QAF 0487 0605 QFA 0506 0508 0513 0522 0553 0558 0564 0574 0593 0595 0603 0695 0705 QTR 0441 0463 0473 0489 0504 0511 0521 0571 0612 0616 0623 0637 0638 0659 0680 0684 SAS 0496 0497 0515 0568 SEU 0501 0635 SWR 0229 0249 0275 0288 0291 0294 0299 0343 0366 TAM 0238 0247 0466 0472 0477 0486 0700 OPERATOR MSN

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# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved (c) Effectivity by MSN and Kit/Configuration The kits and configurations applicable to these MSNs are given at the end of this list: 0012 0017 0030 0037 0045 0050 0054-0055 0059-0060 0062 0064-0067 0069-0073 0077 0082-0083 0086-0087 0095-0096 0098-0100 0102 0106-0107 0109-0113 0116 0118-0122 0127 0132 0138 0140 0143-0144 0148 0153 0155 0162 0165 0171-0172 0177 0181 0183-0184 0188-0189 0191 0195 0198 0200 0203 0205-0206 0209 0211 0219 0222-0224 0226 0229-0232 0234 0238 0240-0241 0244 0247-0251 0253-0256 0258-0259 0261-0262 0265-0267 0269 0271-0272 0275-0277 0279 0281 0283-0288 0290-0291 0293-0296 0299-0301 0303 0305-0306 0308-0309 0311-0317 0320 0322-0324 0326 0328 0330 0333-0334 0337-0340 0342-0346 0348-0351 0353 0356-0358 0361-0362 0364-0366 0368-0370 0372 0375 0380 0382 0384 0386 0388-0389 0392-0393 0396-0398 0400-0401 0403-0405 0407-0409 0412 0418-0423 0425 0427-0428 0432 0437 0439 0441 0443-0444 0448 0451-0452 0454-0456 0458 0461-0463 0465-0466 0469 0472-0473 0476-0477 0479-0481 0484 0486-0487 0489-0491 0493-0494 0496-0498 0500-0513 0515-0516 0518-0519 0521-0522 0524-0527 0529-0530 0532-0533 0535-0536 0539 0542 0548-0553 0555 0558 0564-0565 0567-0568 0570-0571 0573-0574 0576 0578-0579 0581 0584 0587-0588 0591 0593 0595 0597 0600 0602-0603 0605 0607 0609-0610 0612 0614 0616 0618 0620-0621 0623 0625 0627 0629 0631-0638 0640-0642 0644-0645 0647-0650 0652-0667 0669-0671 0673-0676 0678-0680 0682-0684 0686-0688 0690-0693 0695-0697 0699-0701 0703-0705 0707-0709

NOTE : Config. 01 is valid for all the aircraft given in the effectivity of this Service Bulletin. TAP 0308 TCX 0427 0456 THA 0050 0060 0062 0064 0065 0066 0112 0122 0209 0224 0231 0346 THY 0697 0704 TSC 0111 0250 0271 0480 UAE 0248 0251 0283 0293 0295 0314 0316 0326 0328 0345 0348 0365 0372 0382 0384 0392 0396 0409 0437 0451 0452 0455 0462 0491 0494 0509 0518 0525 0536 USA 0315 0323 0333 0337 0342 0370 0375 0380 0388 VKG 0309 0349 0356 0357

KIT No. QTY PER A/C CONFIGURATION 01 OPERATOR MSN

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# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved (3) Spares Servocontrol SC4800-72 SC4800-92 SC4800-10 SC4800-11 B. CONCURRENT REQUIREMENTS If elevator servocontrols PN SC4800-9 are installed on aircraft : accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin or the equivalent production modification: Service Bulletin No. A330-27-3128 Mod. No. 52947S18075 If elevator servocontrols PN SC4800-7A are installed on aircraft : accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin or the equivalent production modification: Service Bulletin No. A330-27-3128 Mod. No. 53386S18200 C. REASON (1) History Further to some reported cases of extrusion and damage of the solenoid valves external preformed packings, a new elevator servocontrol with new capped seals standard has been developed. (2) Objective/Action This Service Bulletin is published to advise all operators of A330 aircraft of the issue of GOODRICH Service Bulletin No. SC4800-27-17. This Service Bulletin recommends modifying the affected servocontrols : — P/N SC4800-72 modified into P/N SC4800-73, — P/N SC4800-92 modified into P/N SC4800-93, — P/N SC4800-10 modified into P/N SC4800-103, — P/N SC4800-11 modified into P/N SC4800-113. (3) Advantages Accomplishment of this Service Bulletin will reinforce the pressure fatigue strength of external packings of the solenoid valves and cancels the action introduced by the paragraph 3.1 of the Airworthiness Directive (AD) F-2004-158.

5

# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved (4) Operational/Maintenance Consequences None D. DESCRIPTION To accomplish this Service Bulletin it is necessary to : (1) Config. 01 NOTE : To accomplish this Service Bulletin you have two possibilities : — either you modify on aircraft the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2, as described in ACCOMPLISHMENT INSTRUCTIONS paragraph B.(1) (a) below, — or you modify on bench them as described in ACCOMPLISHMENT INSTRUCTIONS paragraph B.(1) (b) below. NOTE (01) For the modification of the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2, refer to GOODRICH Service Bulletin No. SC4800-27-17 . (a) In the trimmable horizontal stabilizer trailing edge, modify on aircraft the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 by replacement of the solenoid valve o-ring seals. (b) Modify on bench the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2. E. COMPLIANCE (1) Classification Recommended (2) Accomplishment Timescale Accomplishment of this Service Bulletin is recommended at the earliest opportunity where manpower and facilities are available. F. APPROVAL Approved under the EASA 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.

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# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved 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. Config. 01 , on aircraft, modification of the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2

Config. 01 , on aircraft, replacement of the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2

Config. 01 , on bench

H. WEIGHT AND BALANCE Not changed I. ELECTRICAL LOAD DATA Not changed Get access 2.0 Modification of servocontrols 1.5 Test 1.0 Close-up 2.0 TOTAL MANHOURS 6.5 ELAPSED TIME (HOURS) 6.5

Get access 2.0 Removal/installation of servocontrols 2.0 Test 2.0 Close-up 2.0 TOTAL MANHOURS 8.0 ELAPSED TIME (HOURS) 8.0

Modification of the servocontrols -- TOTAL MANHOURS Refer to GOODRICH Service Bulletin No. SC4800-27-17 ELAPSED TIME (HOURS) Refer to GOODRICH Service Bulletin No. SC4800-27-17

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# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved J. REFERENCES

Service Bulletin No. A330-27-3128 GOODRICH Service Bulletin No. SC4800-27-17 Airworthiness Directive (AD) F-2004-158 K. PUBLICATIONS AFFECTED

L. INTERCHANGEABILITY/MIXABILITY

NOTE : For definitions of interchangeability codes in column INT. refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE (01) Authorized without specific configuration/condition : it is possible to mix old and new P/N on a same aircraft. NOTE (02) Only the mixability configuration(s) and condition(s) stated in this Service Bulletin are approved. Aircraft Maintenance Manual (AMM) : 12-34-24 27-34-51 Elec. Std. Practices Manual (ESPM) : 20-55-00

Illustrated Parts Catalog (IPC) : 27-34-07 27-34-51

DESCRIPTION OLD PART No. NEW PART No. INT MIXABILITY Elevator servocontrol SC4800-72 SC4800-73 01 (01) (02) Elevator servocontrol SC4800-92 SC4800-93 01 (01) (02) Elevator servocontrol SC4800-10 SC4800-103 01 (01) (02) Elevator servocontrol SC4800-11 SC4800-113 01 (01) (02)

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# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved 2. MATERIAL INFORMATION A. MATERIAL — PRICE AND AVAILABILITY (1) Material Modification of removed equipment should be negotiated directly with GOODRICH as per instructions given in Service Bulletin No. SC4800-27-17. (2) Price and Availability Refer to the Vendor Service Bulletin No. SC4800-27-17 for the equipment modification sales terms. B. INDUSTRY SUPPORT INFORMATION Refer to the Vendor Service Bulletin (VSB) for the industry support terms. C. LIST OF COMPONENTS None D. LIST OF MATERIALS — OPERATOR SUPPLIED (1) Consumable Materials None (2) Components

NOTE : For definitions of interchangeability codes in column INT. refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE (01) Modification of removed equipment should be negotiated directly with GOODRICH as per instructions given in Service Bulletin No. SC4800-27-17. E. PARTS TO BE RE—IDENTIFIED BY THE OPERATOR None ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP SC4800-73 4 SRVCNTRL SC4800-72 01 (01) SC4800-93 4 SRVCNTRL SC4800-92 01 (01) SC4800-103 4 SRVCNTRL SC4800-10 01 (01) SC4800-113 4 SRVCNTRL SC4800-11 01 (01)

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# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved F. TOOLING — PRICE AND AVAILABILITY To accomplish this Service Bulletin it is necessary to use the tools listed in AMM 27-34-51 Page block 401. To accomplish this Service Bulletin it is necessary to use the tools listed in GOODRICH Service Bulletin No. SC4800-27-17 . G. SPECIAL TOOLS None

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# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved 3. ACCOMPLISHMENT INSTRUCTIONS A. GENERAL WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). WHEN YOU DO MAINTENANCE WORK, REPAIRS OR MODIFICATIONS, ALWAYS KEEP ELECTRICAL WIRING, COMPONENTS AND THE WORK AREA AS CLEAN AS POSSIBLE. TO DO THIS: — PUT PROTECTION, SUCH AS PLASTIC SHEETING, CLOTHS, ETC.; AS NECESSARY ON WIRING AND COMPONENTS. — REGULARLY REMOVE ALL SHAVINGS, UNWANTED MATERIAL AND OTHER CONTAMINATION. THESE PRECAUTIONS WILL DECREASE THE RISK OF CONTAMINATION AND DAMAGE TO THE ELECTRICAL WIRING INSTALLATION. IF THERE IS CONTAMINATION, REFER TO ESPM 20-55-00. (1) Preparation (a) Config. 01 1 Make sure that the aircraft is electrically grounded (Refer to AMM 12-34-24 Page block 201). 2 For the modification on aircraft of the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 : a Do the preparation procedure as specified in the removal/installation of the elevator servocontrols unit solenoid valves (Refer to AMM 27-34-51 Page block 401). 3 For the modification on bench of the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 : a Do the preparation procedure as specified in the removal/installation of the elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 (Refer to AMM 27-34-51 Page block 401). (2) Standard Practices None B. MODIFICATION (1) Config. 01

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# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved NOTE : To accomplish this Service Bulletin you have two possibilities : — either you modify on aircraft the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2, as described in ACCOMPLISHMENT INSTRUCTIONS paragraph B.(1) (a) below, — or you modify on bench them as described in ACCOMPLISHMENT INSTRUCTIONS paragraph B.(1) (b) below. NOTE (01) For the modification of the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2, refer to GOODRICH Service Bulletin No. SC4800-27-17 . (a) In the trimmable horizontal stabilizer trailing edge, modify on aircraft the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 by replacement of the solenoid valve o-ring seals. NOTE : For the modification of the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2, refer to GOODRICH Service Bulletin No. SC4800-27-17 . 1 Modify each servocontrol. a Remove the two solenoid valves. Refer to AMM 27-34-51 Page block 401. b Replace the seals on both solenoid valves. Refer to GOODRICH Service Bulletin No. SC4800-27-17 . c Install the two solenoid valves. Refer to AMM 27-34-51 Page block 401. (b) Modify on bench the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2. Refer to AMM 27-34-51 Page block 401. NOTE : For the modification of the four elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2, refer to GOODRICH Service Bulletin No. SC4800-27-17 . 1 Remove :

or 4 Elevator servocontrol SC4800-72

4 Elevator servocontrol SC4800-92

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# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved or

or

2 Install :

or

or

or

C. TEST (1) Config. 01 (a) After modification on aircraft of the four elevators servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 : 1 Do the tests after removal/installation of the elevator servocontrols unit solenoid valves (Refer to AMM 27-34-51 Page block 401). (b) After modification on bench of the four elevators servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 : 1 Do an operational test after removal/installation of the elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 (Refer to AMM 27-34-51 Page block 401). D. CLOSE UP (1) Config. 01 (a) After modification on aircraft of the four elevators servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 :

4 Elevator servocontrol SC4800-10

4 Elevator servocontrol SC4800-11

4 Elevator servocontrol SC4800-73

4 Elevator servocontrol SC4800-93

4 Elevator servocontrol SC4800-103

4 Elevator servocontrol SC4800-113

13

# @ A330 SERVICE BULLETIN

DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : Printed in FRANCE © AIRBUS, 2006 All rights reserved 1 Do the close-up procedure as specified in the removal/installation of the elevator servocontrols unit solenoid valves (Refer to AMM 27-34-51 Page block 401). (b) After modification on bench of the four elevators servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 : 1 Do the close-up procedure as specified in the removal/installation of the elevator servocontrols FINs 2CS1, 2CS2, 3CS1 and 3CS2 (Refer to AMM 27-34-51 Page block 401). E. DOCUMENTATION Write in the applicable aircraft records that you have done all the work given in the Service Bulletin.

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# @ A330 SERVICE BULLETIN REPORTING SHEET

5 DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : 1 of 1 Printed in FRANCE © AIRBUS, 2006 All rights reserved TITLE : FLIGHT CONTROLS - ELEVATOR AND HYDRAULIC ACTUATION - INTRODUCE NEW SOLENOID VALVE SEALS ON A330/A340 SERVOCONTROLS. MODIFICATION No. : 53969S18340 53976S18343 53977S18344 53978S18345
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: 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.

# @ A330 SERVICE BULLETIN QUALITY PERCEPTION FORM

5 DATE : Oct 13/05 SERVICE BULLETIN No. : A330—27—3134 REVISION No. : 01 — May 12/06 Page : 1 of 1 Printed in FRANCE © AIRBUS, 2006 All rights reserved 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 X Mod/Inspection X Manpower Operator Supplied 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 Attn : SEM4 Service Bulletins Management FAX : (33) 5 61 93 42 51 Or via your Resident Customer Support Office.