ATR 42/72 - 2010 - - Customer Online

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATRTHALES AVIONICS ELECTRICAL SYSTEMSTECHNICAL PUBLICATIONATR 42/72- 2010 -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

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATRAPPLICABLE TECHNICALPUBLICATION‣ 1. General conditions‣ 2. List of LRU’s‣ 3. Details of evolutions‣ 4. Statement of agreement2

1. GENERAL CONDITIONS2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATRCMM : Component Maintenance Manual.TCMS : Technical Characteristics Maintenance Sheet.SB : Service BulletinSIL : 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’STHALESvendor codeTAES P/NDESCRIPTIONElectronic RotableQty perplaneApplicabilityF0296 156 Transformer E 2 All ATRF0296 102-003-11 DC Generator Control Unit E 2 All ATRF0296 103-003-2 (-11) Hall Effect Current Sensor (HECS) E 5 All ATRF0296105-003-2105-003-1DC Bus Power Control Unit E 1 All ATRF0296 20032-2 Alternator R 2 All ATRF0296 20732 Transformer (DPCT) E 3 All ATRF0296F02962432-112432-30559-012A 559-012B559-012C 559-012DAC Generator Control Unit E 2 All ATRStatic Inverter E 2 All ATRF0296 680-0040-000 Emergency axe - 1 All ATRF0296F02968260-1238260-121945-12945-11DC Starter Generator R 2 All ATRAC Bus Power Control Unit E 1 All ATRF0296 F11NA3121 Transformer Rectifier Unit E 1F0296F0296F46BC0101F46BD0101F96GA0102F96GA0101F0296 B3893-000-500 andETOPS onlyControl Box E 1 All ATRLanding Gear Control Lever E 1 All ATRDC-STAR GSE - Direct CurrentSystem Tester Analyzer RecorderGround Support EquipmentE / All ATR3

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATR3. DETAILS OF EVOLUTIONSSTARTER-GENERATOR P/N 8260-121CMM reference : 24-32-61Revision 9 : Date of update May, 19 th 2008Evolution Reason Application//Brush and bearingreplacementRecommendationsto ATR operators inorder to avoidabnormal MTBURMandatoryduring brushand bearingreplacementOperation,Maintenance,storage,transportation,handling.InProductionsinceSB/ // /SILSIL8260-120-005Rev.7dated 03/09/2009SIL8260-12X-24-007dated 04/1995/Recommendedscheduledmaintenance/ / /SIL8260-12X-24-009Rev. 3dated 06/04/2006/Brush checkprocedure with S/Gfitted on engine./ / /SIL8260-12X-24-010Rev.1dated 09/09/2009/Brush replacementprocedureMandatoryduring brushreplacement/ /SIL8260-12X-24-011Rev. 2dated 10/07/2009//Speed sensortighteningprocedure.Brush and bearingreplacementwithoutdisassembly of theS/G.During eachspeed sensorassemblingoperationMandatoryduring brushand bearingreplacement/ // /SIL8260-12X-24-012Rev 1dated 13/11/2009SIL8260-12X-24-013dated 05/06/2009/Packaging forStarter GeneratorRecommendedfor shipment/ /SIL8260-12X-24-014dated 09/07/2009/ Overhaul procedureMandatoryduring overhaul/SB8260-12X-24-014Rev. 1dated 07/04/2004/AmendmentA, B & C/Do not exist forthis unit/ / /Amendment DImprovement ofreliabilityRecommendedunder repair1989SB8260-120-24-007dated 03/08/1992/4

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATRAC GENERATOR P/N 20032-2CMM reference : 24-22-61Revision 4 : Date of update May, 30th 2008Evolution Reason ApplicationInProductionsinceSBSIL/Verification ofmeasurementUnder repair / /SIL20032-X-24-003dated 06/1993/Verification oftorque valueOn aircraftUnder repair/ /SIL20032-2-24-007dated 28/09/2004/Improvement ofreliabilityUnder repair(overhaul orbearingreplacement)/ /SIL20032-2-24-008dated 24/03/2005Amendment AComponentobsolescenceDuring repair ifcomponent hasto be replaced1988SB20032-2-24-002dated 15/02/1992/Amendment BAmendment CAmendment DAmendment EAmendment FImprovement ofreliabilityImprovement ofrepair procedureImprovement ofreliabilityImprovement ofreliabilityImprovement ofreliabilityDuring repair ofrotating diodesbridges.Under repaironly if rewindingof stator isnecessaryOn customerrequestorif componenthas to bereplaced(P058137)Recommended/On customerrequestorif componenthas to bereplaced(P058137 orP058137A)During repair ifcomponent hasto be replaced1988 / /Onlyunder repairsince 1997/ /1998 / /19991999SB20032-2-24-009Rev. 1dated 03/04/2008SB20032-2-24-005dated 21/12/1998//Amendment GImprovement ofreliabilityDuring repair ifcomponent hasto be replaced1999SB20032-2-24-006dated 21/12/1998/7

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATREvolution Reason ApplicationAmendment HAmendment JImprovement ofreliability &assemblyprocedure.Improvement ofreliability &assemblyprocedure.Qualification of anew source.During repair ifcomponent hasto be replacedDuring repair ifcomponent hasto be replaced(Diode-holderplate assy.)InProductionsince20042007SBSB20032-2-24-007dated 04/12/2002SB20032-2-24-008Rev. 1dated 03/04/2008SIL/SIL20032-2-24-009Rev 1dated 31/03/2008AC GCU P/N 2432-11CMM reference : 24-22-14Revision 4 : Date of update September, 30th 1999Evolution Reason ApplicationAmendment AImprovement ofreliabilityMandatoryduring repair byOEM onlyInProductionsince1988SBSB2432-11-24-002dated 15/02/1992SIL/Amendment BImprovement ofreliabilityMandatoryduring repair byOEM only1988SB2432-11-24-003dated 15/02/1992/Amendment CImprovement ofreliabilityMandatoryduring repair1989 / /Amendment DComponentobsolescenceDuring repair ifPCB orcomponent hasto be replacedSystematicallyduring repair ifPCB Z500 mustbe replacedOnlyunder repairsince 1998SB2432-30-24-001dated 25/04/2006/Amendment EImprovement ofreliabilityDuring repair ifPCB orcomponent hasto be replacedOnlyunder repairsince 1998SB2432-30-24-002Dated 07/12/2009SIL2432-11-24-001dated 15/11/20062432-30Modification forATR72-210version (newpropeller).On customerrequest1994SB2432-30-24-001dated 10/1993/8

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATRAC GCU P/N 2432-30CMM reference : 24-22-14Revision 4 : Date of update September, 30th 1999Evolution Reason ApplicationInProductionsinceSBSIL/Mechanical checkof the rear guidebushing.Under repair / /SIL2432-30-24-001dated 21/06/2007Amendment AComponentobsolescenceDuring repair ifPCB orcomponent hasto be replacedSystematicallyduring repair ifPCB Z500 mustbe replaced1999SB2432-30-24-001dated 25/04/2006/Amendment BImprovement ofreliabilityDuring repair ifPCB orcomponent hasto be replaced1999SB2432-30-24-002Dated 07/12/2009/DC GCU P/N 102-003-11CMM reference : 24-32-11Revision 2 : Date of update July, 5th 2006Evolution Reason ApplicationAmendment AAmendment B/Mechanical checkof the rear guidebushing.Improvement ofreliabilityImprovement ofreliabilityInProductionsinceUnder repair / /Mandatoryduring repair.Recommendedduring repair.19881988SBSB102-003-11-24-001dated 15/02/1992SB102-003-11-24-002dated 15/02/1992SILSIL102-003-11-24-002dated 21/06/2007//Amendment CImprovement ofreliabilityMandatoryduring repair.1988SB102-003-11-24-004dated 15/02/1992/Amendment DImprovement ofreliabilityMandatoryduring repair.2001SB102-003-11-24-005dated 22/12/1999/Amendment EImprovement ofreliabilityMandatoryduring repair.2004SB102-003-11-24-006Rev. 1dated 15/11/2002/9

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATREvolution Reason ApplicationInProductionsinceSBSILAmendment FImprovement ofreliabilityOn customerrequest or ifPCB has to berepaired.2005SB102-003-11-24-007dated 27/01/2005/Amendment G ComponentobsolescenceDuring repair ifselector switchor PCB has tobe replaced2006SB102-003-11-24-008dated 25/04/2006/AC BPCU GCU P/N 945-11CMM reference : 24-41-13Revision 3 : Date of update June, 15th 1999Evolution Reason ApplicationInProductionsinceSBSILAmendment AImprovement ofreliabilityMandatoryduring repair.1989SB945-11-24-002dated 02/1992/945-12Improvement ofreliabilityOn customerrequest.1997SB945-11-24-003dated 30/06/1996/AC BPCU GCU P/N 945-12CMM reference : 24-41-13Revision 3 : Date of update June, 15th 1999Evolution Reason Application/Mechanical checkof the rear guidebushing.InProductionsinceSB/ / /SILSIL945-12-24-001dated 21/06/200710

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATRDC BPCU P/N 105-003-1CMM reference : 24-76-13Revision 3 : Date of update August, 8 th 2006Evolution Reason ApplicationInProductionsinceSBSILAmendment AImprovement ofreliabilityMandatoryduring repair.1994SB105-003-24-003dated 02/1992/Amendment BImprovement ofreliabilityMandatoryduring repair.1994SB105-003-24-004dated 02/1992/Amendment CImprovement ofmanufacturingprocessDuring repair ifcomponent hasto be replaced1994SB105-003-24-005dated 02/1992/Amendment DImprovement ofreliabilityMandatoryduring repair.1994SB105-003-24-006dated 02/1992/Amendment EImprovement ofreliabilityMandatoryduring repair.1994SB105-003-24-007dated 02/1992/Amendment FImprovement ofreliabilityMandatoryduring repair.1994SB105-003-24-001dated 09/1990/Amendment GImprovement ofreliabilityMandatoryduring repair.Onlyunder repairsince 1993/ /Amendment HImprovement ofreliabilityDuring repair ifPCB orcomponent hasto be replacedOnlyunder repairsince 1998SB105-003-24-008dated 21/12/1998/Amendment JImprovement ofreliabilityDuring repair ifPCB has to bereplaced.Onlyunder repairsince 1998/ /Amendment KImprovement ofreliabilityDuring repair ifPCB orcomponent hasto be replacedOnlyunder repairsince 1999SB105-003-24-009dated 21/12/1998/Amendment LImprovement ofreliabilityDuring repair ifPCB orcomponent hasto be replacedOnlyunder repairsince 1999/ /Amendment M ComponentobsolescenceDuring repair ifPCB orcomponent hasto be replacedOnlyunder repairsince 2001/ /Amendment NImprovement ofreliabilityMandatoryduring repair.Onlyunder repairsince 2003SB105-003-24-011dated 12/01/2004/11

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATREvolution Reason ApplicationAmendment PComponentobsolescenceDuring repair ifPCB orcomponent hasto be replacedInProductionsinceOnlyunder repairsince 2004SBSB105-003-24-012dated 25/04/2006SIL/105-003-2Improvement ofreliabilityOn customerrequest.1990SB105-003-24-002dated 02/1992/DC BPCU P/N 105-003-2CMM reference : 24-76-13Revision 3 : Date of update August, 8 th 2006Evolution Reason Application/Mechanical checkof the rear guidebushing.InProductionsinceSB/ / /SILSIL105-003-2-24-001dated 26/06/2007Amendment GImprovement ofreliabilityOn customerrequest.1994 / /Amendment HImprovement ofreliabilityMandatoryduring repair.1994 / /Amendment JImprovement ofreliabilityDuring repair ifPCB orcomponent hasto be replaced1999SB105-003-24-008dated 21/12/1998/Amendment KImprovement ofreliabilityDuring repair ifPCB has to bereplaced.1999 / /Amendment LImprovement ofreliabilityDuring repair ifPCB orcomponent hasto be replaced2000SB105-003-24-009dated 21/12/1998/Amendment MImprovement ofreliabilityDuring repair ifPCB orcomponent hasto be replaced2000 / /Amendment NComponentobsolescenceDuring repair ifPCB orcomponent hasto be replaced2002 / /12

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATREvolution Reason ApplicationAmendment PComponentobsolescenceDuring repair ifPCB orcomponent hasto be replacedInProductionsince2003SBSB105-003-24-010dated 12/01/2004SIL/Amendment RImprovement ofreliabilityMandatoryduring repair.2004SB105-003-24-011dated 12/01/2004/Amendment SComponentobsolescenceDuring repair ifPCB orcomponent hasto be replaced2005SB105-003-24-012dated 25/04/2006/STATIC INVERTER P/N 559-012ACMM reference : 24-21-11Revision 2 : Date of update June, 15th 2001Evolution Reason ApplicationAmendment AAmendment BAmendment CAmendment D/559-012CChecking of overvoltagethresholdprotectionImprovement ofreliabilityImprovement ofthe control of"Static Inverterfault" signalImprovement ofreliability ofauxiliary powercardComponentobsolescenceImprovement ofreliability in orderto avoid doubleloss of staticinverterInProductionsinceUnder repair / /Mandatoryduring repairMandatoryduring repairMandatoryduring repairDuring repair ifPCB orcomponent hasto be replacedMandatoryduring repairSBSILSIL 559-012B-24-001dated 15/06/20061995 / /1995 / /Onlyunder repairsince 1997Onlyunder repairsince 2004Onlyunder repairsince 2009SB559-012A-80-001dated 15/12/1997/ /SB559-012AB-24-002dated 20/02/2009//13

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATRSTATIC INVERTER P/N 559-012BCMM reference : 24-21-11Revision 2 : Date of update June, 15th 2001Evolution Reason ApplicationAmendment AAmendment B/559-012DChecking ofover-voltagethresholdprotectionImprovement ofreliability ofauxiliary powercardComponentobsolescenceImprovement ofreliability inorder to avoiddouble loss ofstatic inverterInProductionsinceUnder repair / /Mandatoryduring repairDuring repair ifPCB orcomponenthas to bereplacedMandatoryduring repair1998SBSB559-012B-80-001dated 13/11/1997SILSIL 559-012B-24-001dated 15/06/20062005 / /2008SB559-012AB-24-002dated 20/02/2009//STATIC INVERTER P/N 559-012CCMM reference : 24-21-11Revision 2 : Date of update June, 15th 2001Evolution Reason ApplicationInProductionsinceSBSIL/ / / / / /STATIC INVERTER P/N 559-012DCMM reference : 24-21-11Revision 2 : Date of update June, 15th 2001Evolution Reason ApplicationInProductionsinceSBSIL/ / / / / /14

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATRT.R.U. P/N F11NA3121CMM reference : 24-32-13Revision / : Date of update October, 15th 1996Evolution Reason ApplicationInProductionsince/ / / / / /SBSILLIGHTING TRANSFORMER P/N 156Technical Characteristics & Maintenance Sheet reference :30-31-13Revision 2 : Date of update June, 1993Evolution Reason ApplicationInProductionsince/ / / / / /SBSILCONTROL BOX P/N F46BC0101CMM reference : 26-15-24Revision 1 : Date of update December, 01st 1993Evolution Reason ApplicationAmendment AAmendment BImprovement ofreliability andfunctionning.Improvement ofmanufacturing &repair processes.Mandatoryunder repair.During repair ifnecessary.InProductionsinceSB1987 / /2009SBF46BC0101-24-001Under validationSIL/CONTROL BOX P/N F46BD0101CMM reference : 26-15-25Revision / : Date of update June, 15th 2001Evolution Reason ApplicationAmendment AImprovement ofreliability.Only underproduction.InProductionsinceSBSIL1996 / /15

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATRLANDING GEAR CONTROL LEVEL P/N F96GA0101CMM reference : 32-31-11Revision 2 : Date of update January, 26th 2009Evolution Reason ApplicationInProductionsinceSBSIL/ / / / / /LANDING GEAR CONTROL LEVEL P/N F96GA0102CMM reference : 32-31-11Revision 2 : Date of update January, 26th 2009Evolution Reason ApplicationAmendment AImprovement offunctionningMandatoryduring repair.InProductionsinceSBSIL1987 / /Amendment BImprovement ofreliabilityOn customerrequest.1989 / /Amendment CImprovement ofreliabilityOn customerrequest.1998SBF96GA0102-24-001dated 21/12/1998/Amendment DImprovement offunctionningDuring repair ifcomponent hasto be replaced.2001 / /TRANSFORMER (DPCT) P/N 20732(DPCT : Differential Protection Current Transformer)Technical Characteristics & Maintenance Sheet reference :24-22-11Revision 2 : Date of update June, 1993Evolution Reason ApplicationInProductionsinceSBSIL/ / / / / /16

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATRHall Effect Captor Sensor P/N 103-003-2Technical Characteristics & Maintenance Sheet reference :24-32-12Revision 4 : Date of update April, 2006Evolution Reason ApplicationAmendment AImprovement ofreliabilityOnly underproductionInProductionsinceSBSIL1998 / /Amendment BImprovement ofreliabilityOnly underproduction2003 / /Amendment CImprovement ofreliabilityOnly underproduction2006 / /EVOLUTION OF Emergency Axe P/N 680-0040-000Technical Characteristics & Maintenance Sheet reference :25-65-01Revision 1 : Date of update 1992Evolution Reason ApplicationInProductionsinceSBSIL/Packaging forEmergency axeRecommendedfor shipment/ /SIL680-0040-000-25-001dated 26/10/2009EVOLUTION OF DC-STAR GSE P/N B3893-000USER MANUAL : Y28-0617Revision a : Date of update October, 17 rd 2008Evolution Reason ApplicationInProductionsinceSBSIL/ / / / / /17

2010 TAES – TECHNICAL PUBLICATIONIssued: February 2010ATR4. 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)18