AIRBUS - 2011 - - Thales Group - Customer Online

2011 TAES - TECHNICAL PUBLICATIONIssued: January 2011AIRBUSTHALES AVIONICS ELECTRICAL SYSTEMSTECHNICAL PUBLICATIONAIRBUS- 2011 -THALES- CUSTOMER SUPPORT DEPARTMENT -41 boulevard de la République – B. P. n° 53 - 78401 CHATOU CEDEX - FRANCETel : 33 1 34.80.73.46 Fax : 33 1 34.80.75.95E-Mail : monique.maximin@fr.thalesgroup.com1

2011 TAES - TECHNICAL PUBLICATIONIssued: January 2011AIRBUSAPPLICABLE TECHNICALDOCUMENTATION‣ 1. General conditions‣ 2. List of LRU’s‣ 3. Details of evolutions‣ 4. Statement of agreement2

2011 TAES - TECHNICAL PUBLICATIONIssued: January 2011AIRBUS1 General ConditionsCMMTCMSSBSIL- Component Maintenance Manual.- Technical Characteristics Maintenance Sheet.- Service Bulletin- Service Information LetterTechnical Publications (CMM/SB/SIL are available. To obtain the sale conditions,contact your Commercial Contact.)Prior to the delivery of a CMM, the customer shall sign a Statement of Agreement.2. List of LRU’sTAES P/N Description Aircraft Type E/RS3716-000 APU STARTER A380 R(3901209-03)F11QY3714 Transformer Rectifier Unit (TRU) A300/A310 EF11QY3121 Transformer Rectifier Unit (TRU) A300/A310 EF34PB6224 Fan A300/A310 RF34PC6224 Fan A300/A310 R8001-2/-3AC Emergency Alternator (Hydraulic A330R(0520952)Driven)152 Auto Transformer A300/A310 E153 Lighting Transformer A300/A310 E154 Lighting Transformer A300/A310 E60-1 Lighting Transformer A300/A310 E61 Lighting Transformer A300/A310 E680-0012-900 Transformer type 129 A300/A310 E680-0021-200 Heat Detector A300/A310 E680-0021-310 Windshield Temperature Regulator A300/A310 E680-0021-320 Windshield Temperature Regulator A300/A310 E680-0021-400 Wind De-Ice Monitor/Control A300/A310 E680-0021-500 Heat Detector A300/A310 E680-1360-100 Auto Windshield Transformer A300/A310 E683-6030-100 Heating Box A300/A310 E683-6027-000 Overheat detector A300/A310 E680-0040-000 Emergency axe ALL684-1024-011/015 Transformer Rectifier unit (TR 880) A330/A340 E1303-2/-3APU Starter A330/A340 R(3888217-3/-4)680-0615-310 TRU (6153A) A300/A310 E700 Auto Transformer A300/A310 E77-1 Lighting Transformer A300/A310 E940 / 940-1 Ground power protection unit A300 EM35AA0104 /AB0102Electrical Warmer A300 E3

2011 TAES - TECHNICAL PUBLICATIONIssued: January 2011AIRBUS3 Details of evolutionsPART: 152, AUTO-TRANSFORMER (A300/A310).DocumentUpdate NumberDate ofUpdateCMM 24-24-11 1st issue 01/04/1973CMM 24-24-11 REV 1 01/10/1973Amendment Reason ApplicationPART: 151A-153-154, LIGHTING TRANSFORMER(A300/A310).DocumentUpdate NumberDate ofUpdateCMM 33-13-22 1st issue 01/04/1973Amendment Reason ApplicationPART: 60-1, LIGHTING TRANSFORMER (A300/A310).DocumentUpdate NumberDate ofUpdateCMM 22-14-38 1st issue 01/04/1973Amendment Reason ApplicationPART: 61, LIGHTING TRANSFORMER (A300/A310).DocumentUpdate NumberDate ofUpdateTCMS 22-12-17 1st issue 01/06/1982Amendment Reason ApplicationPART: 700, AUTO-TRANSFORMER (A300/A310).DocumentUpdate NumberDate ofUpdateCMM 24-22-11 1st issue 01/04/1973Amendt Reason Application4

2011 TAES - TECHNICAL PUBLICATIONIssued: January 2011AIRBUSPART: F11QY3714, TRU (A300/A310).DocumentUpdate NumberDate ofUpdateCMM 24-32-22 1st issue 30/07/03CMM 24-32-22 REV 1 18/12/2003Amendt Reason ApplicationPART: 77A / 77-1, LIGHTING TRANSFORMER (A300/A310).DocumentUpdate NumberDate ofUpdateCMM 33-13-21 1st issue 01/04/1973CMM 33-13-21 REV 1 01/10/1973Amendt Reason ApplicationPART: 940 / 940-1, EXTERNAL POWER PANEL (A300/A310).DocumentUpdate NumberDate ofUpdateCMM 24-41-12 (1st issue) 01/09/1973CMM 24-41-12 REV 3 04/04/1984Amendt. Reason ApplicationSERVICEBULLETINSERVICEBULLETINSERVICEBULLETINSERVICEBULLETINSERVICEBULLETIN940-24-002 01/01/1986 C Reliabiliyimprovement940-24-003 01/05/1988 D To limitthermal effect940-24-004 01/07/1988 B Componentsobsolescence940-24-005 01/02/1992 A Componentsobsolescence940-24-006 25/01/2005 F Improvere-settingfunctionRecommendedRecommendedUpon requestUpon request5

2011 TAES - TECHNICAL PUBLICATIONIssued: January 2011AIRBUSPART: F11QB3121 / F11QY3121, TRANSFORMER RECTIFIERUNIT (A300/A310).DocumentUpdate NumberDate ofUpdateCMM 24-32-11 (1st issue) 15/11/1973CMM 24-32-11 REV 11 15/10/1998Amendt Reason ApplicationSERVICEBULLETINF11QY3121-24-00102/02/98 A To reducethermalconductionaffectin thePCBMandatorySERVICEBULLETINF11QY3121-24-00215/10/2002 B DiodesobsolescenceMandatorySERVICEBULLETINF11QY3121-24-00315/10/2002 Modif toF11QY3714To preventcapacitorBurningMandatorySIL A300-011 25/09/1984SIL F11QB3121-24-0B 01/10/1987SIL F11QB3121-001 01/11/1988SIL F11QB3121 Rev 1 01/03/1991SILSILSILSILSILSILSILSILF11QB3121-24-002F11QB3121-24-003F11QB3121-24-004F11QB3121-24-005 Rev 1F11QB3121-24-006 Rev 1F11QY3121-24-0021 st IssueF11QY3121-24-003 Rev. 1F11QY3121-24-004; 1 st issue -01/11/199401/06/199701/05/199828/02/200131/07/0029/04/9931/07/0011/07/016

2011 TAES - TECHNICAL PUBLICATIONIssued: January 2011AIRBUSPART: 680-0021-200/210/500, OVERHEAT DETECTOR.PART: 680-0021-400, WING DE ICE MONITOR/CONTROL(A300/A310).DocumentUpdate NumberDate ofUpdateAmendt Reason ApplicationCMM 29-09-50 1st issue 31/01/1976CMM 29-09-50 REV 8 15/11/1995PART: 680-0021-300/310/320, WINDSHIELD TEMPERATUREREGULATOR.(A300/A310).DocumentUpdate NumberDate ofUpdateAmendt Reason ApplicationCMM 30-42-11 1 st Issue 25/03/1974CMM 30-42-11 REV 5 30/06/1986SIL 1-79 01/09/1979PART: 680-0615-310, TRANSFORMER RECTIFIER(A300/A310).DocumentUpdate NumberDate ofUpdateAmendt Reason ApplicationCMM 1st Issue 01/03/1983PART: 680-1360-100, SINGLE-PHASE AUTO TRANSFORMER.(A300/A310).DocumentUpdate NumberDate ofUpdateAmendt Reason ApplicationTCMS 30-42-13 1st Issue 01/03/1978TCMS 30-42-13 REV 1 01/02/19948

2011 TAES - TECHNICAL PUBLICATIONIssued: January 2011AIRBUSPART: 683-6027-000, OVERHEAT DETECTOR (A300).DocumentUpdate NumberDate ofUpdateAmendt Reason ApplicationCMM 29-09-52 1st Issue 30/03/1984PART: 683-6030-000/100, FUEL HEATER CONTROL UNIT(A300/A310).DocumentUpdate NumberDate ofUpdateAmendt Reason ApplicationCMM 73-20-02 (1st Issue) 15/09/1983CMM 73-20-02 REV 3 21/09/1988PART: 684-1024-011 / -015, TRANSFORMER RECTIFIER UNIT(A330/A340).DocumentUpdate NumberDate ofUpdateAmendt Reason ApplicationCMM 24-32-31 (1st Issue) 15/10/1993CMM 24-32-31 REV 3 31/03/1998SIL 684-1024***-001 01/04/1995PART: 8001-*, EMERGENCY AC GENERATOR (HYDRAULICDRIVEN)(A330 ETOPS)DocumentUpdate NumberDate ofUpdateAmendt Reason ApplicationCMM 24-22-65 1st Issue 01/05/19929

2011 TAES - TECHNICAL PUBLICATIONIssued: January 2011AIRBUSPART: S3716-000, APU STARTER (A380)DocumentUpdate NumberDate ofUpdateAmendt Reason ApplicationCMM 49-41-11 (1st Issue) 31/05/2007CMM 49-41-11 REV1 28/10/2008SERVICEBULLETINS3716-000-49-001 21/09/1988 Seizing up oftorquelimitationsystemEvery 75 0APUstarts or 6monthsSERVICEBULLETINS3716-000-49-002(Rev1)03/12/2009 Greasing ofthe drivenclutchprocedureRecommendedSERVICEBULLETINS3716-000-49-003(Rev1)03/12/2009 Replacementof the screwsP/NV3004207.RecommendedSILS3716-000-49-001(Rev1)06/05/2010PART: 1303-2/-3, APU STARTER (A340)DocumentUpdate NumberDate ofUpdateAmendt Reason ApplicationCMM 49-41-10(1st Issue)CMM 49-41-10 REV 6 15/12/2004SERVICEBULLETIN1303-49-002(Rev1)04/10/2001 P/N 1303-2becomes1303-3Improvebrush gradeand BrushwearindicatorRecommended10

2011 TAES - TECHNICAL PUBLICATIONIssued: January 2011AIRBUSPART: 680-0040-000, EMERGENCY AXE (ALL)DocumentUpdate NumberDate ofUpdateAmendt Reason ApplicationTCMS 25-65-01 (1st Issue) 1973TCMS 25-65-01 REV 1 1992SIL 680-0040-000-25-00126/10/2009 PackagingforEmergencyaxeRecommendedfor shipment11

2011 TAES - TECHNICAL PUBLICATIONIssued: January 2011AIRBUS4 Statement Of AgreementStatement of Agreement to Terms and Conditions of Sale of Thales TechnicalPublicationsThales Component Maintenance Manual 24-XX-XX is intended solely for use byCompany Name. Copying, reproducing or redistribution of this or any ThalesComponent Maintenance Manual (CMM) or Service Bulletin (SB), to any other party orlocation is strictly prohibited without Thales prior written consent.Thales retains all intellectual property rights, title and interest in the CMMs and/or SBsprovided, including all rights under applicable patents, copyrights, trademarks and tradesecrets, and all renewals and extensions thereto. Company Name shall not alter orremove any patent, copyright, trademark, or proprietary rights notice.Agreed to and Accepted by:____________________________(Print Name)____________________________(Signature)__________________________(Title)__________________________(Date)12