SERVICE BULLETIN REVISION TRANSMITTAL SHEET

**AIRBUS CUSTOMER SERVICES DIRECTORATE**  **1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE**  **Tel : (33) 5 61 93 33 33 Telex : AIRBU 530526F**  **Fax : (33) 5 61 93 42 51** M A N DA T

O RY M A N DA T

O RY M A N DA TO RY M A N D A

TO RY **ATA SYSTEM : 28 TITLE : FUEL - TANKS - INTRODUCE MODIFIED ACT MANHOLE COVER SEAL**  **MODIFICATION No. :** 38036K11669 This page transmits Revision No. 02 of Service Bulletin No. A320-28-1162. A D D I T I O N A L WO R K No additional work is required by this revision for aircraft modified by any previous issue. R E A S O N This Revision is issued to : - add the aircraft MSN 0827, 0891, 1868, 2247 and 2290 to the effectivity, - add figure for A319 configuration. C H A N G E S SUMMARY : - EFFECTIVITY

. Operators updated. PLANNING INFORMATION : - EFFECTIVITY

. 1.A. Aircraft MSN 0827, 0891, 1868, 2247 and 2290 added to the effectivity. Operators updated. - COMPLIANCE - Accomplishment Timescale

. 1.E.(2) Timescale updated. ACCOMPLISHMENT INSTRUCTIONS : - MODIFICATION DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 1 of 2 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN REVISION TRANSMITTAL SHEET

. 3.B.(1)(a) Figure reference added. . 3.B.(1)(b) Figure reference added. - Figure 2

. Figure added. NOTE : Layout changes due to computerization of this revision are not identified. F I L I N G I N S T R U C T I O N S 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. H I S T O R Y O F P R E V I O U S R E V I S I O N S Revision No. 01 was issued to : - inform the operators that, for aircraft under warranty, AIRBUS will credit the material and the manhours. - add aircraft MSN 0870, 1670 and 2165 to the effectivity. R E V I S I O N S E Q U E N C E ORIGINAL : Feb 06/08 REVISION No. : 01 - Jul 16/08 REVISION No. : 02 - Dec 18/09

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 2 Printed in France © AIRBUS 2008 All rights reservedSERVICE 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 M A N DA T

O RY M A N DA T

O RY M A N DA TO RY M A N DA TO RY **ATA SYSTEM : 28 TITLE : FUEL - TANKS - INTRODUCE MODIFIED ACT MANHOLE COVER SEAL**  **MODIFICATION No. :** 38036K11669 R E A S O N /D E S C R I PT I O N /O P E R A T I O N A L C O N S E Q U E N C E S Leakages have been found at the seal of the outer manhole cover of the Additional Center Tank (ACT). This Service Bulletin details the procedure to replace the existing manhole cover seal by a new seal. The accomplishment of this Service Bulletin will prevent leakage at the outer manhole cover seal.

EVALUATION TABLE COMPLIANCE Mandatory 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 No KIT PRICE (USD) See SB

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

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MODIFICATION CLASSIFICATION MAJOR 38036K11669

MINOR None
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. **E F**  **F E**  **C T**  **I V**  **I T** **Y** This Service Bulletin is applicable to this (these) operator(s) : 03X 17W 31X 39Z 47W 52W 53U 53Z 57W 59U 80X 91X 93V 95W AAF AAR ABQ ACA AFR AHY AJM AMU AUH BEC BER BIE BMA BRS CEF DCS DGA EIN EZY G4I HDA HVN JBU JKK KAC KFR KNE KYV KZR LMJ LTU LVG MEA MLM MON MSR NKS NVR OHY ORF QAF QTR R1T RJA SHJ SHY SVR SVW TAI TAP TAR TCX THY TOM TRK TWJ UKN USA VKG VUN WGT WHT C O N C U R R E N T R E Q U I R E M E N T S Config. 01 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) or the equivalent production modification(s): Service Bulletin No. A320-28-1105 Mod. No. 31935K7740 NOTE : Before the accomplishment of this Service Bulletin, it is necessary to introduce the new manhole cover PN D2827106620000 with Mod. No. 31935K7740 (Fuel - Tanks - Introduce a new outer manhole cover with new seal) or Service Bulletin A320-28-1105 (Introduce new manhole cover and seal). R E F E R E N C E S/ R E P E R C U S S I O N S TFU : 28.11.37.001 OEB : None AOT : None SIL : None LIFE LIMIT : None LINE MAINTENANCE AFFECTED : No OTHERS : None DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

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N A T U R E O F T H E WO R K AIRCRAFT : YES EQUIPMENT : NO HARD : NO SOFT : NO OBRM : NO M A N P OW E R Kit 281162D01R00

**TOTAL MANHOURS 14.50 ELAPSED TIME (HOURS) 14.50**  NOTE : The manpower data refer to one ACT. Manpower may differ depending on number of ACTs installed. M A T E R I A L I N F O R M A T I O N AIRCRAFT DATA Config. 01 Outer manhole cover seal. A P P E N D I C E S None

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

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DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

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**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** M A N DA T

O RY M A N DA T

O RY M A N DA TO RY M A N DA TO RY **ATA SYSTEM : 28 TITLE : FUEL - TANKS - INTRODUCE MODIFIED ACT MANHOLE COVER SEAL**  **MODIFICATION No. :** 38036K11669 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. P L**  **A N**  **N I**  **N G**  **I N**  **F O**  **R M**  **A T**  **I O**  **N A. E**  **F F**  **E C**  **T I**  **V I**  **T Y**  (1) Models 319-112 319-114 319-115 319-132 319-133 320-212 320-214 320-232 321-211 321-231 (2) Aircraft (a) Effectivity by MSN This Service Bulletin is applicable to aircraft MSN : 0633 0663 0666 0668 0677 0680 0687 0715 0725 0775 0781 0802 0808 0811 0815 0823 0827 0841 0852 0870 0891 0910 0927 0956 0963 0991 0993 1002 1006 1008 1017 1024 1042 1053 1157 1204 1212 1219 1227 1233 1238 1250 1256 1276 1333 1335 1366 1403 1412 1417 1425 1431 1436 1442 1447 1451 1455 1462 1465 1468 1472 1479 1481 1485 1492 1496 1499 1503 1517 1519 1521 1525 1531 1536 1539 1556 1589 1602 1607 1611 1623 1629 1632 1638 1651 1656 1666 1670 1690 1695 1701 1704 1707 1711 1720 1724 1726 1727 1748 1763 1772 1783 1794 1795 1811 1843 1850 1868 1878 1880 1881 1887 1905 1908 1921 1926 1928 1932 1941 1946 1950 1953 1960 1966 1967 1970 1972 1984 1988 1999 2005 2021 2041 2046 2060 2105 2107 2117 2165 2190 2192 2211 2213 2216 2226 2228 2234 2246 2247 2259 2263 2279 2280 2284 2286 2290 2307 2314 2336 2341 2403 2410 2421 2440 2456 2476 2487 2507 2550 2553 2566 2590 2592 2610 2650 2653 2675 2682 2687 2706

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2707 2716 2730 2748 2793 2799 2801 2837 2862 2921 2949 2974 3005 3013 3022 3046 3065 3073 3085 3096 3106 3133 3164 3198 3199 3243 3260 3274 3315 3355 (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 03X 2421 17W 3046 31X 2192 39Z 0956 47W 3164 52W 3243 53U 1727 1880 53Z 1468 57W 1999 59U 2706 3073 80X 2748 91X 2837 93V 1589 95W 2949 AAF 0808 0823 1006 1451 AAR 0802 1227 2041 2226 2247 2290 ABQ 1008 ACA 1602 1611 1623 1632 1638 1726 1748 1772 1783 1811 AFR 2213 2228 2279 2456 2716 3065 AHY 2487 AJM 1503 1905 DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

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OPERATOR MSN AMU 1850 1926 AUH 2403 BEC 3199 BER 1629 1966 1988 2005 BIE 0827 0891 2707 BMA 1690 1711 2190 2653 2799 BRS 2263 CEF 2801 3085 DCS 1053 DGA 1485 1556 EIN 0815 0841 0991 EZY 2682 3106 G4I 1157 1795 2507 HDA 0633 0993 1024 1695 1984 2021 HVN 2974 3005 3013 3022 3198 3315 3355 JBU 2246 2259 2280 2284 2286 2307 2314 2336 JKK 1276 1333 1366 1843 1946 KAC 2046 KFR 2650 KNE 2165 KYV 2117 KZR 1042 1204 LMJ 1868 LTU 1607 LVG 1950 1970 MEA 1878 1953 1967 DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

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OPERATOR MSN MLM 2592 MON 1707 1763 1794 1941 2105 2234 MSR 0680 0687 0715 0725 NKS 2476 2590 NVR 2211 2216 2410 OHY 0663 0668 0963 ORF 2566 QAF 0927 1335 QTR 1656 1928 2107 2341 3274 R1T 1908 RJA 2730 2793 SHJ 0910 SHY 0811 1670 SVR 1720 SVW 2921 3133 TAI 2553 2610 2687 2862 TAP 0870 TAR 1479 3096 TCX 0677 1238 1250 2060 THY 1002 1219 1233 TOM 0781 0852 TRK 0666 0775 TWJ 2550 UKN 3260 USA 1403 1412 1417 1425 1431 1436 1442 1447 1455 1462 1465 1472 1481 1492 1496 1499 1517 1519 1521 1525 1531 1536 1539 1651 1666 1701 1704 1724 DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

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OPERATOR MSN VKG 1881 1887 1921 1932 1960 1972 VUN 1017 WGT 1212 WHT 1256 2440 2675 (c) Effectivity by MSN and Kit/Configuration The Kits and configurations applicable to these MSNs are given at the end of this list 0633 0663 0666 0668 0677 0680 0687 0715 0725 0775 0781 0802 0808 0811 0815 0823 0827 0841 0852 0870 0891 0910 0927 0956 0963 0991 0993 1002 1006 1008 1017 1024 1042 1053 1157 1204 1212 1219 1227 1233 1238 1250 1256 1276 1333 1335 1366 1403 1412 1417 1425 1431 1436 1442 1447 1451 1455 1462 1465 1468 1472 1479 1481 1485 1492 1496 1499 1503 1517 1519 1521 1525 1531 1536 1539 1556 1589 1602 1607 1611 1623 1629 1632 1638 1651 1656 1666 1670 1690 1695 1701 1704 1707 1711 1720 1724 1726-1727 1748 1763 1772 1783 1794-1795 1811 1843 1850 1868 1878 1880-1881 1887 1905 1908 1921 1926 1928 1932 1941 1946 1950 1953 1960 1966-1967 1970 1972 1984 1988 1999 2005 2021 2041 2046 2060 2105 2107 2117 2165 2190 2192 2211 2213 2216 2226 2228 2234 2246-2247 2259 2263 2279-2280 2284 2286 2290 2307 2314 2336 2341 2403 2410 2421 2440 2456 2476 2487 2507 2550 2553 2566 2590 2592 2610 2650 2653 2675 2682 2687 2706-2707 2716 2730 2748 2793 2799 2801 2837 2862 2921 2949 2974 3005 3013 3022 3046 3065 3073 3085 3096 3106 3133 3164 3198-3199 3243 3260 3274 3315 3355 KIT No. QTY PER A/C CONFIGURATION None 01 NOTE : Config. 01 is valid for all the aircraft given in the effectivity of this Service Bulletin as a standard configuration. (3) Spares None **B. C O**  **N C**  **U R**  **R E**  **N T**  **R E**  **Q U**  **I R**  **E M**  **E N**  **T S**  Config. 01 Accomplishment of this Service Bulletin requires the prior or simultaneous accomplishment of the following Service Bulletin(s) or the equivalent production modification(s) : Service Bulletin No. A320-28-1105 Mod. No. 31935K7740 NOTE : Before the accomplishment of this Service Bulletin, it is necessary to introduce the new manhole cover PN D2827106620000 with Mod. No. 31935K7740 (Fuel - Tanks - DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

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Introduce a new outer manhole cover with new seal) or Service Bulletin A320-28-1105 (Introduce new manhole cover and seal). **C. R E** **A S**  **O N**  (1) History Leakages have been found at the seal of the outer manhole cover of the Additional Center Tank (ACT). (2) Objective/Action This Service Bulletin details the procedure to replace the existing manhole cover seal by a new seal. (3) Advantages The accomplishment of this Service Bulletin will prevent leakage at the outer manhole cover seal. (4) Operational/Maintenance Consequences The accomplishment of this Service Bulletin can prevent an ACT auto transfer failure. **D. D E**  **S C**  **R I**  **P T**  **I O**  **N** To accomplish this Service Bulletin it is necessary to : (1) Config. 01 (a) Remove the outer manhole cover seal. (b) Install the outer manhole cover seal. (c) Re-identify the ACTs. **E. C O**  **M P**  **L I**  **A N**  **C E**  (1) Classification Mandatory (2) Accomplishment Timescale Threshold : Within 3000 Flight Cycles or 24 months after the effective date of the AD, 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 given above but reference should be made to the AD for confirmation of the mandated accomplishment timescale.

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

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**F. A P**  **P R**  **O V**  **A L**  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. M A**  **N P**  **O W**  **E R**  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 Get Access 6.00 Modification 1.50 Test 1.00 Close-up 6.00 **TOTAL MANHOURS 14.50 ELAPSED TIME (HOURS) 14.50**  NOTE : The manpower data refer to one ACT. Manpower may differ depending on number of ACTs installed. **H. W E**  **I G**  **H T**  **A N**  **D B** **A L** **A N**  **C E**  Not changed **I. E L**  **E C**  **T R**  **I C**  **A L**  **L O** **A D**  **D A** 

**T**

**A** Not changed **J. R E**  **F E**  **R E**  **N C**  **E S**  Aircraft Maintenance Manual (AMM) : 20-28-00 28-00-00 28-11-27 28-11-37 28-28-00 Elec. Std. Practices Manual (ESPM) : 20-55-00 Consumable Material List (CML) Standards Manual (SM) DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

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Service Bulletin No. A320-28-1105 **K. P U**  **B L**  **I C**  **A T**  **I O**  **N S**  **A F**  **F E**  **C T**  **E D**  Aircraft Maintenance Manual (AMM) : 28-11-37 Illustrated Parts Catalog (IPC) : 28-11-02 28-11-04 28-11-27 28-11-37 **L. I N**  **T E**  **R C**  **H A**  **N G**  **E A**  **B I**  **L I**  **T Y**  **/ M**  **I X** **A B**  **I L**  **I T** **Y** DESCRIPTION OLD PART No. NEW PART No. INT MIXABILITY ACT1 (A319CJ) D2827105100600 D2827105101000 01 Not applicable ACT1 (A319CJ) D2827105100800 D2827105101000 01 Not applicable ACT2 (A319CJ) D2827105200600 D2827105201000 01 Not applicable ACT2 (A319CJ) D2827105200800 D2827105201000 01 Not applicable ACT3 (A319CJ) D2827105300600 D2827105301000 01 Not applicable ACT3 (A319CJ) D2827105300800 D2827105301000 01 Not applicable ACT4 (A319CJ) D2827105401000 D2827105401800 01 Not applicable ACT4 (A319CJ) D2827105401400 D2827105401600 01 Not applicable ACT4 (A319CJ) D2827105401200 D2827105401600 01 Not applicable ACT5 (A319CJ) D2827105500600 D2827105501000 01 Not applicable ACT5 (A319CJ) D2827105500800 D2827105501000 01 Not applicable ACT6 (A319CJ) D2827105600600 D2827105601000 01 Not applicable ACT6 (A319CJ) D2827105600800 D2827105601000 01 Not applicable ACT1 (A319, A320) D2827091101000 D2827091101200 01 Not applicable ACT2 (A319, A320) D2827091101000 D2827091101200 01 Not applicable ACT1 (A319, A320) D2827091100800 D2827091101400 01 Not applicable ACT2 (A319, A320) D2827091100800 D2827091101400 01 Not applicable ACT1 (A321) D2827091300600 D2827091301000 01 Not applicable ACT2 (A321) D2827091300600 D2827091301000 01 Not applicable ACT1 (A321) D2827091300800 D2827091301200 01 Not applicable ACT2 (A321) D2827091300800 D2827091301200 01 Not applicable ACT1 (A321) D2827107500400 D2827107500800 01 Not applicable ACT2 (A321) D2827107500400 D2827107500800 01 Not applicable ACT1 (A321) D2827107500600 D2827107500800 01 Not applicable ACT2 (A321) D2827107500600 D2827107500800 01 Not applicable NOTE : For definitions of interchangeability codes in column INT. refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE : The old ACT PNs are those applicable after accomplishment of the Service Bulletin A320-28-1105.

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

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**2. M A**  **T E**  **R I**  **A L**  **I N**  **F O**  **R M**  **A T**  **I O**  **N A. M**  **A T**  **E R**  **I A**  **L -**  **P R**  **I C**  **E A**  **N D**  **A V** 

**A I**  **L A**  **B I**  **L I**  **T Y**  (1) Material Vendor parts are to be purchased from : PFW Aerospace AG Am Neuen Rheinhafen 10 D-67346 Speyer GERMANY For ordering by internet: http://www.pfw.aero For ordering by tel.: +49 62 32 616 4404 For ordering by e mail: Customer-support@pfw.aero For ordering by fax: +49 62 32 616 4702 (2) Price and Availability Sales terms for the equipment must be negotiated with the equipment vendor. **B. I N**  **D U**  **S T**  **R Y**  **S U**  **P P**  **O R** **T I**  **N F**  **O R**  **M A**  **T I**  **O N**  For aircraft under warranty at 03 Dec 2007, AIRBUS will credit the material and the manhours indicated in this Service Bulletin at the operator’s agreed in-house warranty labor rate upon receipt of a warranty claim. **C. L I**  **S T**  **O F**  **C O**  **M P**  **O N**  **E N**  **T S**  None **D. L I**  **S T**  **O F**  **M A**  **T E**  **R I**  **A L**  **S -**  **O P**  **E R**  **A T** **O R**  **S U**  **P P**  **L I**  **E D**  (1) Consumable Materials DESCRIPTION REFERENCE TO CML QTY PER A/C INST/DISP MAT No. Oil Mat. No. 03-008 As required Zinc chromate Mat. No. 05-002 As required Leak detector Mat. No. 05-071 As required Coating (Blue Color) Mat. No. 07-001D As required Acid anodizing Mat. No. 13-002 As required Polyurethane top coat, grey Mat. No. 16-002 As required Epoxy primer Mat. No. 16-006 As required (2) Components ITEM NEW PART No. QTY UM KEYWORD ITEM OLD PART No. INT INST DISP

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2 282P140000-000 1 Seal (2) D2827105920000 01 NOTE (01) NOTE : Discard. NOTE : The quantity of the seals is per ACT. NOTE : For definitions of interchangeability codes in column INT. refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. **E. P A**  **R T** **S T** **O B**  **E R**  **E -**  **I D**  **E N**  **T I**  **F I**  **E D**  **B Y**  **T H**  **E O**  **P E**  **R A**  **T O**  **R** ITEM NEW PART No. KEYWORD ITEM OLD PART No. INT D2827105101000 ACT1 D2827105100600 01 NOTE (01) D2827105101000 ACT1 D2827105100800 01 D2827105201000 ACT2 D2827105200600 01 NOTE (01) D2827105201000 ACT2 D2827105200800 01 D2827105301000 ACT3 D2827105300600 01 NOTE (01) D2827105301000 ACT3 D2827105300800 01 D2827105401600 ACT4 D2827105401200 01 NOTE (01) D2827105401600 ACT4 D2827105401400 01 D2827105401800 ACT4 D2827105401000 01 NOTE (01) D2827105501000 ACT5 D2827105500600 01 NOTE (01) D2827105501000 ACT5 D2827105500800 01 D2827105601000 ACT6 D2827105600600 01 NOTE (01) D2827105601000 ACT6 D2827105600800 01 D2827091101400 ACT1 D2827091100800 01 NOTE (01) D2827091101200 ACT1 D2827091101000 01 NOTE (01) D2827091101400 ACT2 D2827091100800 01 NOTE (01) D2827091101200 ACT2 D2827091101000 01 NOTE (01) D2827091301000 ACT1 D2827091300600 01 NOTE (01) D2827091301200 ACT1 D2827091300800 01 NOTE (01) D2827091301000 ACT2 D2827091300600 01 NOTE (01) D2827091301200 ACT2 D2827091300800 01 NOTE (01) D2827107500800 ACT1 D2827107500400 01 NOTE (01) D2827107500800 ACT1 D2827107500600 01 D2827107500800 ACT2 D2827107500400 01 NOTE (01) D2827107500800 ACT2 D2827107500600 01 NOTE : For definitions of interchangeability codes in column INT. refer to ATA Common Support Data Dictionary (CSDD), Chapter 2. NOTE(01) Before the accomplishment of this Service Bulletin, it is necessary to introduce the new manhole cover PN D2827106620000 with Mod. No. 31935K7740 (Fuel - Tanks - Introduce a new outer manhole cover with new seal) or Service Bulletin A320-28-1105 (Introduce new manhole cover and seal). **F. T O**  **O L**  **I N**  **G -**  **P R**  **I C**  **E A**  **N D**  **A V** 

**A I**  **L A**  **B I**  **L I**  **T Y**  None

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**G. S P**  **E C**  **I A**  **L T** **O O**  **L S**  None

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DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 12 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN

**3. A C**  **C O**  **M P**  **L I**  **S H**  **M E**  **N T**  **I N**  **S T**  **R U**  **C T**  **I O**  **N S**  **A. G E**  **N E**  **R A**  **L** WARNING : MAKE SURE THAT YOU OBEY ALL THE WARNINGS AND ALL THE CAUTIONS INCLUDED IN THE REFERENCED PROCEDURES. WARNING : MAKE SURE THAT YOU HAVE THE CORRECT FIRE FIGHTING EQUIPMENT AVAILABLE BEFORE YOU START ANY TASK ON THE FUEL SYSTEM. WARNING : MAKE SURE THAT THE GROUND SAFETIES AND THE CHOCKS ARE IN POSITION ON THE LANDING GEAR. WARNING : MAKE SURE THAT THE GROUND SAFETIES AND THE NOTICES ARE IN POSITION ON THE FLIGHT CONTROLS. WARNING : BEFORE POWER IS SUPPLIED TO THE AIRCRAFT MAKE SURE THAT ELECTRICAL CIRCUITS UPON WHICH WORK IS IN PROGRESS ARE ISOLATED. WARNING : OBEY THE SAFETY PROCEDURES WHEN YOU DO WORK IN THE FUEL TANK. WARNING : DO NOT GET AIRCRAFT FUEL : - IN YOUR MOUTH - IN YOUR EYES - ON YOUR SKIN FOR A LONG TIME WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL. AIRCRAFT FUEL IS POISONOUS AND CAN GO THROUGH YOUR SKIN INTO YOUR BODY. IF YOU ARE CONTAMINATED WASH WITH CLEAN WATER AND IF NECESSARY GET MEDICAL HELP. WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START THE DEFUEL/REFUEL PROCEDURE. IN THE SAFETY AREA, DO NOT : - SMOKE - MAKE SPARKS OR FIRE - USE ANY EQUIPMENT THAT IS NOT APPROVED FOR REFUEL/DEFUEL PROCEDURES. AIRCRAFT FUEL IS FLAMMABLE. CAUTION : REMOVE FUEL LEAKAGE IMMEDIATELY. CAUTION : APPLY A LIGHT FILM OF OIL (Mat. No. 03-008) TO THE INNER LINING OF THE BLADDER TANK, IF THE ACT IS TO STAY WITHOUT FUEL FOR MORE THAN 20 DAYS. CAUTION : ALWAYS OBEY THE PRECAUTIONS THAT FOLLOW TO KEEP ELECTRICAL WIRING IN A SATISFACTORY CONDITION (ELECTRICALLY AND MECHANICALLY SERVICEABLE). DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 13 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN

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 ELECTRICAL 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 Do the fuel safety procedures of the fuel tank (Refer to AMM 28-00-00, Page block 201). 2 Remove the ACT from the aircraft (Refer to AMM 28-11-27, Page block 401). (2) Standard Practices (a) Refer to the AIRBUS Standards Manual (SM) 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. The SM will give you the correct part number to part number relationship. (b) For material specifications (Mat. No.) given in this Service Bulletin, refer to the Consumable Material List (CML) . (c) For electrical bonding (Refer to AMM 20-28-00, Page block 201). (d) Install bolts and washers with Zinc chromate (Mat. No. 05-002). (e) Apply Coating (Blue Color) (Mat. No. 07-001D) to the bonding points. (f) Apply Acid anodizing (Mat. No. 13-002), Epoxy primer (Mat. No. 16-006) and Polyurethane top coat, grey (Mat. No. 16-002) to the outer surface and edge of the manhole. (g) For the leak test of the outer manhole cover, use Leak detector (Mat. No. 05-071). **B. M O**  **D I**  **F I**  **C A**  **T I**  **O N**  (1) Config. 01 (a) Remove the outer manhole cover seal. Refer to Figure 1, A319CJ, ACT Configuration Refer to Figure 2, A319, ACT Configuration DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 14 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN

Refer to Figure 3, A320, ACT Configuration Refer to Figure 4, A321, ACT Configuration Refer to Figure 5 Refer to AMM 28-11-37, Page block 401 1 Remove from the ACT : Refer to Figure 5, Sheet 1, Detail A, BEFORE 1 Cover D2827106620000 Item (1) Retain 1 Seal D2827105920000 Item (2) Discard

with : 44 Bolt Item (3) Retain 42 Washer Item (4) Retain

2 Washer Item (5) Retain

NOTE : Make marks on the bolts, Item (3), and washers, Item (5), to make sure that you will install them in the same positions. (b) Install the outer manhole cover seal. Refer to Figure 1, A319CJ, ACT Configuration Refer to Figure 2, A319, ACT Configuration Refer to Figure 3, A320, ACT Configuration Refer to Figure 4, A321, ACT Configuration Refer to Figure 5 Refer to AMM 28-11-37, Page block 401 CAUTION : THE NEW SEAL, ITEM 2, MUST NOT BE BENT. HANDLE WITH CARE. CAUTION : THE SEAL PN 282P140000-000, ITEM 2, THAT IS USED ONE TIME CANNOT BE USED AGAIN. INSTALL ALWAYS NEW SEALS. CAUTION : A DAMAGED SEAL, ITEM 2, MAY NOT BE FITTED. NOTE : The seal face of the manhole area must be clean and without damage. 1 Carefully open the packing of the delivered seal. 2 Put the manhole cover, Item (1), and the seal, Item 2, adjacent to each other on the work table. 3 Do not lift the seal, Item 2. Only pull the seal carefully horizontally over the cardboard box onto the manhole cover. Align the seal, Item 2, fully with the drilled holes in the manhole cover, Item (1). 4 Put the bolts, Item (3), in the holes No. 17 and No. 20 of the manhole cover, Item (1). Then lift the manhole cover, Item (1), with the bolts, Item (3). 5 Put in position and install on the ACT wall : DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 15 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN

Refer to Figure 5, Sheet 2, Detail A, AFTER 1 Seal 282P140000-000 Item 2 1 Cover D2827106620000 Item (1) Retained

with : 2 Bolt Item (3) Retained 2 Washer Item (4) Retained

and tighten the two bolts, Item (3), lightly by hand. 6 Install in a diametrical sequence : Refer to Figure 5, Sheet 3, Detail B 42 Bolt Item (3) Retained 40 Washer Item (4) Retained

2 Washer Item (5) Retained

and tighten the bolts, Item (3), lightly by hand. NOTE : The bolts, Item (3), with marks and the washers, Item (5), must be installed in the same position. 7 Torque the bolts, Item (3), to 3.0 Nm (2.214 lb.ft) in a diametrical sequence. Refer to Figure 5, Sheet 3, Detail B 8 Torque the bolts, Item (3), to 4.0 Nm (2.952 lb.ft) in a diametrical sequence. Refer to Figure 5, Sheet 3, Detail B 9 Torque the bolts, Item (3), to 5.0 Nm (3.690 lb.ft) in a diametrical sequence. Refer to Figure 5, Sheet 3, Detail B 1 0 Wait 2 hours for the seal to expand, to mould and to settle into place. 1 1 Then torque the bolts, Item (3), to 5.0 Nm (3.690 lb.ft) in a diametrical sequence. Refer to Figure 5, Sheet 3, Detail B (c) Re-identify the ACTs. (Refer to Para. 2.E. PARTS TO BE RE-IDENTIFIED BY THE OPERATOR). **C. T E**  **S T**  (1) Config. 01 (a) Do the leak test of the ACT outer manhole cover (Refer to AMM 28-28-00, Page block 501). DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 16 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN

(b) Do the electrical bonding test of the outer manhole cover of the ACT (Refer to AMM 20-28-00, Page block 201). **D. C L**  **O S**  **E U**  **P** (1) Config. 01 (a) Make sure that the work areas are clean and clear of tools and other items of equipment. (b) Install the ACT in the aircraft (Refer to AMM 28-11-27, Page block 401). (c) Do the tests after installation of the ACT (Refer to AMM 28-11-27, Page block 401). (d) After installation of the ACT, do the operational test of the fuel transfer pump pressure switch (Refer to AMM 28-28-00, Page block 501). **E. D O**  **C U**  **M E**  **N T**  **A**

**T I**  **O N**  Write in the applicable aircraft records that you have done all the work given in the Service Bulletin.

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 17 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN

Figure 1, Sheet 1 Config. 01 : A319CJ, ACT Configuration

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 18 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN

Figure 2, Sheet 1 Config. 01 : A319, ACT Configuration DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 19 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN

Figure 3, Sheet 1 Config. 01 : A320, ACT Configuration

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 20 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN

Figure 4, Sheet 1 Config. 01 : A321, ACT Configuration

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 21 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN

Figure 5, Sheet 1 Config. 01 : Removal/Installation of the Seal

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 22 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN

Figure 5, Sheet 2 Config. 01 : Removal/Installation of the Seal

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 23 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN

Figure 5, Sheet 3 Config. 01 : Removal/Installation of the Seal

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 24 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN REPORTING SHEET

**TITLE : FUEL - TANKS - INTRODUCE MODIFIED ACT MANHOLE COVER SEAL MODIFICATION No. :**  38036K11669 P l e a s e c o m p l ete t h e a p p ro p r i ate i te m (A o r B ) : A - SB W I L L B E embodied .................................................................. YES/NO (if NO please comment) If YES, aircraft concerned (as per SB effectivity by default) and planned dates (month/year) of embodiement:

............................................................................................................................... ..............................................

............................................................................................................................... .............................................. B - SB H AS B E E N embodied on aircraft: ............................................................................................................

............................................................................................................................... ..............................................

............................................................................................................................... .............................................. Operator comments:..............................................................................................................

..............................

............................................................................................................................... ..............................................

............................................................................................................................... .............................................. From Airline: ...................................................................................................................

..................................... Name/Title: ....................................................................................................................

...................................... Signature:..................... Date: ..................................................... I f o p e rat i o n a l d o c u m e n t at i o n i s affe cte d ( s e e Pa ra g ra p h 1

. K of t h i s S B ) : If information is needed prior to next normal revision or prior to SB embodiment, please indicate required service(s): Either : Advance data................................................................................... YES/NO Or : Intermediate/Temporary revision ..................................................... YES/NO I m p o rt a n t I n fo r m at i o n : 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. P l e a s e re t u r n t h i s c o m p l ete d s h e e t to : **AIRBUS CUSTOMER SERVICES DIRECTORATE**  **1 Rond Point Maurice Bellonte 31707 BLAGNAC CEDEX FRANCE**  Attn: SEDCC1 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 : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 1 of 1 Printed in France © AIRBUS 2008 All rights reservedSERVICE BULLETIN REPORTING QUALITY

**TITLE : FUEL - TANKS - INTRODUCE MODIFIED ACT MANHOLE COVER SEAL MODIFICATION No. :**  38036K11669 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 futher 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 C o m m e n ts :

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

DATE : Feb 06/08 SERVICE BULLETIN No. : A320-28-1162

REVISION No. : 02 - Dec 18/09 Page : 1 of 1 Printed in France © AIRBUS 2008 All rights reserved