SERVICE INFORMATION LETTER

Transcription

1 CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0) TELEX AIRBU F AIRBUS SERVICE INFORMATION LETTER SUBJECT: Centralized Fault Display System (CFDS) Anomalies CHAPTER: 00 AIRCRAFT TYPE: A318, A319, A320, A321 APPLICABILITY: All Aircraft 0. REASON FOR REVISION: Update of data. See Section 5 for detailed list of evolutions. Procedure to download SIL and associated files from AOLS. 1. PURPOSE: The present SIL identifies all the known CFDS anomalies/bite deviations. It is intended to be used by maintenance engineering as a synthetic document, providing a short description of each deviation, as well as the affected part and the corrective action, with a cross-reference to the relevant TFU/TSM procedure. The fault messages/warnings or behaviours which should be known by line maintenance teams, are covered by the Trouble Shooting Manual. More precisely, the messages/behaviours described in this SIL are those for which the conditions of occurrence are precise/known and reproducible. In addition are mentioned messages/behaviours for which a statistical survey revealed a too high number of occurrences (more than 1 every 5 flights per aircraft without any logbook complaint). The last part of this SIL gives the filter content. Each operator is responsible for uploading and updating the filter database, according to the part numbers of equipment fitted on their aircraft. SIL NUMBER: PAGE: 1 of 9 + Appendix CREATION DATE: v 30/1989 REVISION: 29 REVISION: DATE: 31-MAR-06

2 CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0) TELEX AIRBU F AIRBUS SERVICE INFORMATION LETTER 2. RECOMMENDATIONS The appendix is divided into five parts, which are: A. The list of PFR failure messages (internal and external) which request specific maintenance action. B. The list of ECAM WARNINGS and MAINTENANCE STATUS shown on the PFR, which request specific maintenance action. C. The list of CLASS 3 failure messages which request specific maintenance action. D. The anomalies related to the general use of the CFDS. E. The list of messages/warnings which AIRBUS recommend to filter. ta 1: The classification criteria of data recorded in A, B, C, D, E of this document is the chapter associated to the message/anomaly. Each page of parts A, B, C, D indicates: 1. The chapter of the message or anomaly. 2. The description of the message which is considered as non justified under some conditions. 3. Specific maintenance action to be performed or some remarks about the anomaly. 4. The computer affected by the anomaly. 5. The Part Number (P/N) of the affected computer. 6. The corrective P/N. 7. The reference of the TFU/TSM to obtain more details about the anomaly. 8. The A/C type involved. 9. The indication whether AIRBUS recommended (Y) or not (N) to filter a message/warning. ta 2: New/revised items are highlighted by a vertical adjacent NEW in the margin. ta 3:Lower-case letters such as i or j represent a variable integer (usually 1, 2, or 1 to 3). i and j are used in the messages. X represents any alphanumeric character in the part numbers SIL NUMBER: PAGE: 2 of 9 + Appendix CREATION DATE: v 30/1989 REVISION: 29 REVISION: DATE: 31-MAR-06

3 CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0) TELEX AIRBU F AIRBUS SERVICE INFORMATION LETTER ta 4:For each item, carefully check that the part number fitted on your aircraft corresponds to the affected P/N mentioned in the SIL. Otherwise, the remark is not applicable to your A/C. Each page of part E indicates: 1. The chapter of the message or warning to be filtered if applicable. 2. The first line of the message or warning to be filtered if applicable. 3. The second line of the message or warning to be filtered if applicable. 4. The Flight phase criteria if applicable. 5. The source criteria if applicable. 6. The P/N which is concerned by the anomaly. 7. The name of the part which is concerned by the anomaly. ta 5:A character _ means that a space has to be entered on the MCDU or in MFT. ta 6:To prevent duplication of messages in the filter content, a character $ is used instead of the position number where the computer is installed i.e. VHF $ instead of VHF 1, VHF 2, VHF 3. ta 7: Anytime the P/N of a computer is changed on the A/C, it is recommended to update the filter content, using information which are in Part E of this SIL. ta 8: Part E of this SIL - Filter Content - is available on floppy disk - called FilenvXX.320 (XX: Revision number). For customization, refer to Maintenance Filter Tool (MFT) - SIL MATERIAL INFORMATION t Applicable 4. PROCUREMENT INFORMATION t Applicable SIL NUMBER: PAGE: 3 of 9 + Appendix CREATION DATE: v 30/1989 REVISION: 29 REVISION: DATE: 31-MAR-06

4 CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0) TELEX AIRBU F AIRBUS SERVICE INFORMATION LETTER 5. LIST OF EVOLUTIONS PART ITEMS TYPE REMARK A FMGCi (1CAj)/RMPi (1RGi)/ILSi (1RTi) Revised Wording A HF1 COUPLER (4RE1)/FEEDER HF1 (6RE1)/ANTENNA (5RE1) New A DU ND CAPT(3WK1)/ND CAPT POT(8WK1) New A DU ND FO(3WK2)/ND FO POT(8WK2) New A DU PFD CAPT(1WK1)/PFD CAPT POT(7WK1) New A DU PFD FO(1WK2)/PFD FO POT(7WK2) New A DU EWD(2WK1)/ECP(6WM) New A DU SD(2WK2)/ECP(6WM) New A QUALIFIER Di/WXRj (1SQj) (i = 1 or 2 and j = 1 or 2) New A ADIRUi+3(1FPi+3) ADRBUS/WXRj(1SQj) (i = 1 or 2 and j = 1 or 2) Revised Wording + P/N A WXRi (1SQi) (i = 1 or 2) New A DMCi: NO WXRj CHj D (i = 1, 2 or 3 and j = 1 or 2) Revised Wording A DMC(i): NO TCAS D (i = 1 or 2) Revised Wording + P/N A FWC(i): NO D FROM TCAS (i = 1 or 2) Revised Wording + P/N A NO TCAS D Revised Wording + P/N A ATC(i): NO D FROM TCAS (i = 1 or 2) Revised Wording + P/N A TCAS (1SG) Revised Wording + P/N A QUALIFIER Ci/WXRj (1SQj) (i = 1 or 2 and j = 1 or 2) New A ATCi (1SHi)/TCAS (100SG) source TCAS (i = 1 ou 2) New A NO ATCi D source CFDS (i = 1 or 2) Revised Wording + P/N A ATCi (1SHi)/TCAS (1SG) source TCAS (i = 1 ou 2) Revised Add TFU ref. B 2161 AIR:PACK i REGUL FAULT Revised Wording B 3443 NAV TCAS FAULT Revised Add TFU ref. C CFDIU (1TW)/WXRi (i = 1 or 2) New C ADIRU3 (1FP3) ADR BUS/WXRi (1SQi) (i = 1 or 2) New E 2161 AIR_PACK_1$2_FAULT Revised Wording E E E E E DU_ND_CAPT(3WK1)/ ND_CAPT_POT(8WK1) DU_ND_FO(3WK2)/ ND_FO_POT(8WK2) DU_PFD_CAPT(1WK1)/ PFD_CAPT_POT(7WK1) DU_PFD_FO(1WK2)/ PFD_FO_POT(7WK2) DU_EWD(2WK1)/ ECP(6WM) SIL NUMBER: PAGE: New New New New New 4 of 9 + Appendix CREATION DATE: v 30/1989 REVISION: 29 REVISION: DATE: 31-MAR-06

5 CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0) TELEX AIRBU F AIRBUS SERVICE INFORMATION LETTER E DU_SD(2WK2)/ ECP(6WM) New E ADIRU$($FP$)_IR_BUS/ WXR$($SQ$) New E ADIRU$$$($FP$$$)_ADRBUS/ WXR$($SQ$) New E NO_ATC_$_D Revised Wording + P/N 6. PROCEDURE TO DOWNLOAD FILES ATTACHED TO SIL ON AOLS 1/ Procedure to download SIL.pdf files: - under Technical Publication select Engineering Technical Documentation, - select Document Type and SIL Number then click on the SEARCH button, - once selected SIL is opened, it is possible either to print or to save on disk. 2/ Procedure to download attached files to SIL : Following files can be downloaded through the Airbus OnLine Services (AOLS) FTP: - AIRBUS Filter Envelop (FILENVxx.320 [xx=rev]), - AIRBUS FILTER DBASE label to be stuck onto the floppy. Procedure to download: - select FTP Site under General Services menu, - click on ASSOCIATED DOCUMENTS for SIL under the main ROOT, - select the SIL folder to access the package content. te that Filter Envelop used for A320, A330 and A340 require the Maintenance Filter Tool (MFT). Please refer to SIL which explains how to install MFT. SIL NUMBER: PAGE: 5 of 9 + Appendix CREATION DATE: v 30/1989 REVISION: 29 REVISION: DATE: 31-MAR-06

6 CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0) TELEX AIRBU F AIRBUS SERVICE INFORMATION LETTER LIST OF ABREVIATIONS SIGLUM TITLE ACARS ACSC ACP ADIRU ADF ADR AEVC AFS AIDS AMM AMU AOA APU ASSY ATC A/P A/THR ATIMS BCL BITE BMC BSCU CAM CFDIU CFDS CHC CIDS CPC CVC C/B DC DFDR DLRB DLS DMC DME Aircraft Communication Addressing & Reporting System Air Conditionning System Controler Audio Control Panel Air Data Inertial Reference Unit Automatic Direction Finder Air Data Reference Avionic Equipment Ventilation Controller Auto Flight System Aircraft Integrated Data System Aircraft Maintenance Manual Audio Management Unit Angle-Of-Attack Auxiliary Power Unit Assembly Air Transport Association Air Traffic Control Autopilot Auto Thrust Air Traffic and Information Management System Battery Charge Limiter Built-in Test Equipment Bleed Monitoring Computer Braking & Steering Control Unit Cabin Assignment Module Centralized Fault Detection Interface Unit Centralized Fault Display System Cargo Heat Controller Cabin Intercommunication Data System Cabin Pressure Controller Cargo Ventilation Controller Circuit Breaker Direct Current Digital Flight Data Recorder Data Loader Routing Box Data Loader Selector Display management Computer Distance Measuring Equipment SIL NUMBER: PAGE: 6 of 9 + Appendix CREATION DATE: v 30/1989 REVISION: 29 REVISION: DATE: 31-MAR-06

7 CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0) TELEX AIRBU F AIRBUS SERVICE INFORMATION LETTER SIGLUM TITLE DMCU DMU DU Drain Mast Central Unit Data Management Unit Display Unit ECAM ECB ECS ECU EFDU EIU ELAC EVMU FADEC FAC FCD FCDC FCOM FCU FCV FDIMU FDIU FG FIN FL FM FMGC FMGS FMS FQI CH FQIC FT FWC FWD F/CTL F/D GCU GPWC GPCU GW HF HP HPV HUD Electronic Centralized Aircraft Monitor Electronic Control Box Environmental Control System Engine Control Unit Engine Fire Detection Unit Engine Interface Unit Elevator Aileron Computer Engine Vibration Monitoring Unit Full Authority Digital Engine Control Flight Augmentation Computer Flight Control Display Flight Control Data Concentrator Fuel Control and Management Computer Flight Control Unit Flow control Valve Flight Data Interface Management Unit Flight Data Interface Unit Flight Guidance Functional Item Number Flight Level Flight Management Flight Management & Guidance Computer Flight Management & Guidance System Flight Management System Fuel Quantity Indicator Channel Fuel Quantity Indication Computer Feet Flight Warning Computer Forward Flight Control Flight Director Ground Control Unit Ground Proximity Warning Computer Ground Power Control Unit Gross Weight High Frequency High Pressure High Pressure Valve Head Up Display SIL NUMBER: PAGE: 7 of 9 + Appendix CREATION DATE: v 30/1989 REVISION: 29 REVISION: DATE: 31-MAR-06

8 CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0) TELEX AIRBU F AIRBUS SERVICE INFORMATION LETTER SIGLUM TITLE Head Up display Computer Instrument Landing System Integrated Standby Instrument System Landing Gear control & Interface Unit Low Oil Pressure Line Replacement Unit Line Replacement Unit Landing Gear HUDC ILS ISIS LGCIU LOP LRU L/G M MCDU MEL MFT MLG MM MMEL MPD MRB MSN MTBF MTBR MTBUR MU ND NLG NM OBRM OVHT PA PC PCU PDU PES PFD PFR PHC PRAM PRV PTT PTU P/N QAR RA RFI Mach Number Multi-purpose Control and Display Unit Master Equipment List Maintenance Filter Tool Main Landing Gear Maintenance Manual Master Minimum Equipment List Maintenance Planning Document Maintenance Review Board Manufacturer Serial Number Mean Time Between Failures Mean Time Between Removal Mean Time Between Unscheduled Removal Management Unit Navigation Display se Landing Gear Nautic Miles On Board Replaceable Module Overheat Public Address Pack Controller Power control Unit Power Distribution Unit Passenger Entertainment System Primary Flight Display Post Flight Report Probe Heat Computer Pre-Recorded Announcement and Music Pressure Regulator Valve Push-To-Talk Power Transfer Unit Part Number Quick Access Recorder Radio Altimeter Request For Information SIL NUMBER: PAGE: 8 of 9 + Appendix CREATION DATE: v 30/1989 REVISION: 29 REVISION: DATE: 31-MAR-06

9 CUSTOMER SERVICES DIRECTORATE 1 ROND POINT MAURICE BELLONTE BLAGNAC CEDEX FRANCE TELEPHONE + 33 (0) TELEX AIRBU F AIRBUS SERVICE INFORMATION LETTER SIGLUM TITLE RFR RMP SB Request For Revision Radio Management Panel Service Bulletin SDAC SDCU SDI SEC SFCC SFCS SFE SIL SRM TAT TBD TEM TFU THS TLT TPIU TRU TSM ULD UPPR CRG DET VHF VOR WAI WAIV WDB WHC WRX ZC System Data Acquisition Concentrator Smoke Detection Control Unit Spares Data Improvement Spoiler Elevator Computer Slat/Flap Control Computer Slat/Flap Control System Supplier Furnished Equipment Service Information Letter Structural Repair Manual Turn Around Time To Be Defined Tool and Equipment Manual Technical Follow-Up Trimmable Horizontal Stabilizer Temperature Limitation Thermostat Tyre Pressure Indicating Computer Transformer Rectifier Unit Trouble Shooting Manual Unit Load Device Upper Cargo Smoke Detector Very High Frequency VHF Omnidirectional Range Wing Anti-Ice Wing Anti-ice Valve Wall Disconnect Box Window Heat Computer Weather Radar Transceiver Zone Controller SIL NUMBER: PAGE: 9 of 9 + Appendix CREATION DATE: v 30/1989 REVISION: 29 REVISION: DATE: 31-MAR-06

10 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref NO D NO MAINT. ACTION CFDIU B401ACM0505 B401ACM0506 Filter Associated P/N : FWD CARGO FAN OR SPLY 6H NO MAINT. ACTION if power supply between FAN and CVC is OK, 115 V 3 phases. (Minimum value : 110 V) CVC TFU Associated P/N : AFT CARGO FAN OR SPLY 35 NO MAINT. ACTION if power supply between FAN and CVC is OK, 115 V 3 phases. (Minimum value : 110 V) CVC TFU Pi FLOW CONTROL VALVE Associated to Maintenance Status PACK 1(2), NO MAINT. ACTION if Bite test OK Associated P/N : FCV 751A A TFU Associated P/N : EIUi : NO ZONE CONT P(S) D Associated with ECAM warning : ENG1(2) BLEED STATUS FAULT. NO MAINT. ACTION ZC 775A A TFU / TFU / TSM 75 Associated P/N : EIU CFMI Part A : page 1

11 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref EIUi NO ZONE CONT P(S) D NO MAINT. ACTION If not associated to Maintenance Status : ENG1(2)EIU EIU TFU / TFU / TSM 71 Filter Associated P/N : NO ZONE CTL D NO MAINT. ACTION, Could be intermittent (INTM). ZC 775A A TFU SDACi: NO D FROM ECS i Associated P/N : CFDIU B401ACM0404 NO MAINT. ACTION if occurs in phase 6 ZC 775A A TFU Associated P/N : DMCi : FACj D Maintenance action DMC ALL P/N (Soft std DMC V50) Associated P/N : FCU (2CA) BUS CP-L/ WRX 1 (1SQ1) If no logbook associated logbook complaint, maintenance action is required. RADAR Soft 05 Associated P/N : Part A : page 2

12 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref FCU(2CA)CP-L BUS/ WXRi(1SQi) (i = 1 or 2) maintenance action required if no logbook complaint. RADAR Filter FCU(2CA)CP-R BUS/ WXRi(1SQi) (i = 1 or 2) Associated P/N : maintenance action required if no logbook complaint. RADAR Associated P/N : FCU(3CA)CP-L BUS/ WXRi 1SQi (I=1 or 2) NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect. RADAR FCU(3CA)CP-R BUS/ WXRi 1SQi (I=1 or 2) NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect. Associated P/N : RADAR RADARi:NO D FROM EFIS i PANEL Associated P/N : NO MAINT. ACTION if no log book complaint RADAR VSB WRT-701X VSB WRT-701X Associated P/N : Part A : page 3

13 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref AFS:MCDUi NO MAINT. ACTION if no log book complaint FMGC ALL P/N NONE TFU Filter Associated P/N : MDCU3(3CA3)/ATSU1(1TX1) maintenance action if MCDU 3 not installed. Can be filtered if MCDU 3 not installed ATSU host platform S/W LA2T0S111C1B0F1 LA2T0J13000C0F1 TFU Associated P/N : AFS:FMGC$(DO NOT REMOVE) NO MAINT. ACTION FAC FAC pre Std B397BAM0617 B397BAM AFS:FMGCi NO MAINT ACTION IF MESSAGE NOT ASSOCIATED WITH ANY ECAM WARNING AND COCPIT EFFECT FMGC Associated P/N : FMGC PEGA C13042xA01 B546BAM0203 B546CCM0101 B546CAM0101 B398AAM0410 B398BAM0207 Associated P/N : AFS:FMGCi (FMi) NO MAINT. ACTION if no log book complaint FMGC B398AAM0408 B398BAM0205 B398BCM0104 B546BAM0206 B546CAM0102 B546CCM0104 B546BCM0205 C13042AA01 B398AAM0409 B398BAM0206 B398BCM0106 TFU TFU Associated P/N : Part A : page 4

14 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref AFS:FMGCi/ATHR ENGD FDBK NO MAINT. ACTION if not associated with ECAM WARNING : AUTO FLT A/THR OFF. FMGC (LEGAC Y) B398AAM0xxx B398BAM0xxx B398BCM0xxx TBD Filter FMGCi (1CAi)/ RMPi(1RGi)/ILSi(2RTi) Associated P/N : maintenance action if not logbook complaint ILS X202 (Allied) (Collins) TBD (Allied) (Collins) Associated P/N : FMGCi(1CAi) BUS MMR/ MMRi (40RTi) Reset MMR1 when I equal 1 (Reset MMR2 when i equal 2). If in the Ground Scanning "FMGC BUS ILS/MMR" or in the TSD "PORT B RX FAIL" are visible carry out associated TSM task. MMR VSB Collins GLU TSM task /871 Associated P/N : FMGCi(1CAj)/ RMPi(1RGi)/ILSi(1RTi) maintenance action if no FM auto reset reported in the logbook. FMGC All P/N N/A SIL & SIL Associated P/N : FMGECi(1CAi)/ RMPi(1RGi)/ILSi(1RTi) maintenance action if no logbook entry ILS (Collins) N/A Associated P/N : Part A : page 5

15 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref DIR1 (101RH)/OBRM Maintenance advise: A CIDS interface and power-up test must be performed to confirm validity of the failure and to clear the failure message from the ground report. CIDS DIR Z064H000030F Z064H000031A Z064H000031B TBD (end 2005) Filter Associated P/N : CHECK HF (i) ANTENNA CIRCUIT NO MAINT ACTION if no log book entry HF TRANSC EIVER VSB HFS TFU Associated P/N : ICAO ADDRESS/HFi(3REi) NO MAINT. ACTION. This message is triggered if Datalink not activated (MOD 31286) and CFDIU Label 157 not received within 30s after HFDR power-up. This message is associated with CLASS3 Fault message " ATSU(1TX1)/ HFi(3Ri)" HFDR Collins HFS900D TBD Associated P/N : HF1 COUPLER(4RE1)/ FEEDER HF1(6RE1)/ANTENNA(5RE) maintenance action if no logbook compaint. COUPLE R Associated P/N : HFDRi(3REi)/ATSU1(1TX1) Source ACARS MU NO MAINT. ACTION when HFDR not activated and CFDIU PRE STD 9B (Source name "ACARS MU" in the PFR) ATSU HOST Platform S/W LA2T0J13000C0F1 LA2T0J13002C0F1 C12860AA02 TFU Associated P/N : CFDIU B401ACM0507 Part A : page 6

16 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref NO HF 1 D Source CFDS Maint. Action if triggered in phase 02. HF Transcei ver TBD Filter Associated P/N : CHECK VHF 1 ANTENNA CIRCUIT NO MAINT. ACTION if VSB mentioned in Corrective P/N not incorporated. VHF VSB VHF VSB VHF TFU Associated P/N : NO VHF3 D NO MAINT. ACTION when VHF3 not installed CFDS C12860AA02 CFDIU STD 10 TBC (STD 9B) Associated P/N : VHF 3 TRANSCEIVER NO MAINT. ACTION if no log book complaint VHF VSB VHF Associated P/N : VHF0(1RC0) NO MAINT. ACTION if occurs in phase 02 VHF N/A Associated P/N : Part A : page 7

17 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref RMPi(1RGi)/RMPj(1RGj) NO MAINT. ACTION required RMP C12848AA01 TBD C12848CA01 Filter Associated P/N : SDU1(5RV1)/ATSU1(1TX1) Generated by ATSU when SATCOM not installed. Disregard when SATCOM not installed (This message may be displayed on PFR, System Test and Ground scanning). ATSU host platform S/W LA2T0S162C0C0F1 LA2T0S111C1B0F1 TFU Associated P/N : FAP1 (120RH)/ DIR2/CAM Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous. CIDS SDF Z064H000030F Z064H000031A Z064H000031B TBD (end 2005) Associated P/N : FAP1 (120RH)/DIR1/CAM Maintenance advise: To check the validity of the FAP failure message, please select the FAP status page. Should any anomaly is visible on subject page, please refer to the corresponding trouble shooting task. CIDS DIR Z064H000030F Z064H000031A Z064H000031B TBD (end 2005) Associated P/N : FAP1 (120RH)/DIR2/CAM Maintenance advise: To check the validity of the FAP failure message, please select the FAP status page. Should any anomaly is visible on subject page, please refer to the corresponding trouble shooting task. CIDS DIR Z064H000030F Z064H000031A Z064H000031B TBD (end 2005) Associated P/N : Part A : page 8

18 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref AAP (126RH) ATT 4L Maintenance advise: If an AAP failure message is recorded into the PFR, perform a visual check of the AAP operation to determine the validity of the fault message. CIDS DIR Z064H000030F Z064H000031A Z064H000031B Filter Associated P/N : AAP (126RH) ATT 4L/ DEU B (300RH7) Maintenance advise: If an AAP failure message is recorded into the PFR, perform a visual check of the AAP operation to determine the validity of the fault message. CIDS DIR Z064H000030F Z064H000031A Z064H000031B Associated P/N : AIP (320RH1) ATT 1L Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous. CIDS SDF Z064H000030F Z064H000031A Z064H000031B TBD (end 2005) Associated P/N : AIP (320RH9) ATT 4L Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous. CIDS SDF Z064H000030F Z064H000031A Z064H000031B TBD (end 2005) Associated P/N : CIDS2(102RH) NO MAINT. ACTION. Associated with MAINT STATUS TEMP CTL 1 and TEMP CTL 2. problem of a discrete label status computed by the CIDS2 and used by ACSC 1 and 2. ACSC 1803A TBD EYDCC Technical note P2161ME V1 Associated P/N : Part A : page 9

19 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref DIR1 (101RH) -SDF Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous. CIDS SDF Z064H000030F Z064H000031A Z064H000031B TBD (end 2005) Filter Associated P/N : DIR1 (101RH) BUS/ DIR2 (102RH) Maintenance advise: A CIDS interface and power-up test should be performed to confirm validity of the failure message. The associated time may be completely erroneous. CIDS SDF Z064H000030F Z064H000031A Z064H000031B TBD (end 2005) Associated P/N : NO CIDS 1(2) D Please refer to TFU CIDS Z010H000abcd abcd=3113 or 3117 or 5115 or 5117 or 5118 or 5119 or 520A or 521A Associated P/N : ALL P/N NO CIDS 1(2) D (INTM) Please refer to TFU CIDS Z010H000abcd abcd= 3113 or 3117 or 5115 or 5117 or 5118 or 5119 or 520A or 521A Associated P/N : ALL P/N 24 P-OW-ER CONSUMPTION NO MAINT ACTION if no log book complaint BCL 35-0L TBD TFU CFDS TBD TFU CFDS 35-0L TFU Associated P/N : Part A : page 10

20 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref POWER SUPPLY INTERRUPT NO MAINTENANCE ACTION ILS Filter Associated P/N : POWER SUPPLY INTERRUPT Source EIS 1(2)(3) Maintenance action if occurs during PWR transfer: Phase 01 and 02 (Engine start-up), Phase 09 and 10 (Engine Shut Down). DMC EIS II Soft SXT3F-E2SA-0410 SXT3C-E2SA-0420 EIS II Soft Std S5 Associated P/N : IDGi DISCONNECTED Check Class 3 Fault messages. GPCU A B (SB ) TFU / TSM 24 Associated P/N : IDGi OIL LEVEL SENSOR/ GCUi - Source EPGS Quality issue affecting component inside the GCU. Ony GCUs manufactured before v 2002 are affected. When message is triggered, the GCU should be removed and sent to vendor Hamilton Sundstrand for repair. GCU J TFU Associated P/N : AFS:28V PWR 11XU1 MAINT. ACTION if occurs during PWR transfer: Phase 02 (Engine start-up), Phase 09 and 10 (Engine Shut Down) FMGC All P/N N/A Associated P/N : Part A : page 11

21 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref CHECK GCU APU PIN C1, C5 GEN APU PIN A9, A10 1.If associated with a generator trip : remove the APU generator, otherwise, NO MAINT.ACTION. 2.If APU GEN FAULT imediately after APU start,reset APU GEN P/B SW. on OVHD panel. GCU A B C (SB ) TFU Filter SDACi: NO TR1 CURRENT 1PU1 Associated P/N : At APU start NO MAINT. ACTION SDAC 35-0E E E TFU SDACi : NO D FROM BCLi Associated P/N : NO MAINT. ACTION if no Log Book complaint. SDAC 35-0E E E Associated P/N : SLIDE BTL XY/ DEU B (300RHZ) with X=1, 3 or 4 and Y=R or L and Z=1, 6 or 8. maintenance action required. CIDS DIR Z064H000030F Z064H000031A Z064H000031B Associated P/N : WRG: CAN BUS A (or B) NO MAINT. ACTION if fault message displayed after a reset of CIDS or CIDS-SDF CIDS DIR Z064H000030D Z064H000030E Z064H000030F TBD SIL Associated P/N : Part A : page 12

22 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref CHECK FDU ENGi SUPPLY NO MAINT. ACTION if no log book complaint FDU TFU Filter Associated P/N : CHECK FDU APU LOOP A WARN CKT MAINT. ACTION if APU FDU test does not confirm the fault message FDU TBD TFU Associated P/N : CHECK FDU APU LOOP B WARN CKT MAINT. ACTION if APU FDU test does not confirm the fault message FDU TBD TFU Associated P/N : SDCU CHANNEL 2 (10WQ) NO MAINT. ACTION if reset of the SDCU clears the message SDCU RAI-2800-M0706 SB TFU Associated P/N : SFCC1(2) or FLP PPU POWER If associated with failure message FLP1(2) PCU VALVEBLOCK 23(24) CV. Corrective action: replace SFCC at the origin of the fault. SFCC From S/N 5813 To S/N 5956 OIT /05 Associated P/N : Part A : page 13

23 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref SFCCi or FLAP PPU POWER - If recorded in PFR without associated warning, NO MAINTENANCE ACTION required. If recorded in the PFR with the associated Ecam Warning: "F/CTL FLAP SYSi FAULT" or "F/CTL FLAP LOCKED" performed a manual reset of the SFCC through the SFCC MCDU BITE menu: SFCC/WTB RESET SLT/FLT CSU 51CV OR WIRING TO SLT1(2)/FLP1(2) If recorded in PFR without warning MAINT. ACTION required. If Warning refer to TFU SFCC SFCC (S/N 1732 to 1934) (S/N 1743 to 1904) Associated P/N : TFU Amdt. A TFU Filter Associated P/N : SDACi: NO D FROM SFCC NO MAINT ACTION if no log book complaint SDAC 35-0E E E Associated P/N : FLP1(2) PCU VALVEBLOCK 23(24) CV If associated with failure message SFCC1(2) or FLP PPU POWER. Corrective action: replace SFCC at the origin of the fault. SFCC From S/N 5813 To S/N 5956 OIT / SFCCi or SLAT PPU POWER If recorded in PFR without warning: NO MAINTENANCE ACTION required. If associated with Ecam Warning: "F/CTL SLAT SYSi FAULT" or "F/CTL SLAT LOCKED" performed a SFCC/WTB reset through the MCDU. SFCC Associated P/N : (S/N 1727 to 1906) TFU Associated P/N : Part A : page 14

24 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref 2800 FUEL L(R) XFR VALVE OPEN If this ECAM message is reported, perform functional BITE test of the ICTVs - FLSS Status (AMM ) and a functional BITE test of the low-level sensors - FLSS BITE (AMM ). further action is required, if both test of the FLSS status and FLSS BITE show NO FAULT FUEL QUANTITY FQIC 3QT NO MAINT. ACTION if FQIC grades remains at 1 after FQIC test through CFDS. associated with ECAM warning : FQI CH1(2) FAULT FQIC FQIC Associated P/N : SIC5059-xx-xx05 SIC5059-xx-xx06 TFU SIC5059-xx-xx07 TFU Filter Associated P/N : FUEL LEVEL SENSING L (or R) UNFULL SENSOR 25QJ1 (or 25QJ2 or 26QJ1 or 26QJ2) NO MAINT. ACTION if triggered in flight phase 02 FLSCU ALL P/N TBD Associated P/N : R(L) WAI FILTER OR VALVE 10DL (9DL) NO MAINT. ACTION if not associated with ECAM warning. ZC 775A A TFU / TSM 30 Associated P/N : DRAINMAST HEATER FWD AFT NO MAINT. ACTION if no blockage or system malfunction reported. DMCU H H H882 SB TFU Associated P/N : Part A : page 15

25 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref DRAINMAST HEATER FWD/AFT Replace the drainmast even if the fault is not confirmed on ground. This deviation has been identified. A correction will be incorporated in the next Drainmast DRAIN MAST H H882 SB TFU Filter Associated P/N : DRAINMAST HEATER MID Valid only if Mod embodied. NO MAINT. ACTION if no blockage or system malfunction reported. DMCU H H H882 SB TFU / Associated P/N : DRAINMAST HEATER MID Valid only if Mod embodied. Replace the drainmast even if the fault is not confirmed on ground. This anomaly has been identified. A correction will be incorporated in the next Drainmast. DRAIN MAST H H882 SB TFU Associated P/N : BAD D FROM CFDIU NO MAINT. ACTION ILS VSB ILS AI S/B: Associated P/N : CFDIU B401ACM CFDIU(1TW)/HF(i) (3REi) maintenance action if no logbook complaint. HF Transcei ver TBD Associated P/N : Part A : page 16

26 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref LGCIU: NO D FROM CFDS Appears after a CFDIU power down, NO MAINTENANCE ACTION LGCIU A4A A4B TFU Filter Associated P/N : RADAR x: NO D FROM CFDIU NO MAINT. ACTION RADAR VSB RTA-4A TFU Associated P/N : QAR NO MAINT. ACTION if mentioned in Phase 1 in last leg report FDIU B B3 TFU QAR TAPE LOW NO MAINT. ACTION if mentioned in Phase 1 in last leg report FDIU Associated P/N : B B3 TFU Associated P/N : DFDR NO MAINT. ACTION if mentioned in Phase 1 in last leg report FDIU B B3 TFU Associated P/N : Part A : page 17

27 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref DFDR PLAYBACK NO MAINTENANCE ACTION. RECOMMENDED STEP: EMBODY VSB SFIM FDIU/ FDIU ED43A1D3 ED43A1D4 Filter Associated P/N : SSFDR NO DMU D (INTM) Maintenance Action required DMU Associated P/N : DAR Maintenance Action required DMU Associated P/N : DAR TAPE LOW Maintenance Action required DMU Associated P/N : DU EWD(2WK1)/ECP(2WM) maintenance action required if no logbook complaint. EIS II Software SXT3CE2SA0420 SXT4EE2SA050A TBD Associated P/N : Part A : page 18

28 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref DU ND CAPT(3WK1)/ ND CAPT POT(8WK1) maintenance action required if no logbook complaint. EIS II Software SXT3CE2SA0420 SXT4EE2SA050A TBD Filter Associated P/N : DU ND FO(3WK2)/ ND FO POT(8WK2) maintenance action required if no logbook complaint. EIS II Software SXT3CE2SA0420 SXT4EE2SA050A TBD Associated P/N : DU PFD CAPT(1WK1)/ PFD CAPT POT(7WK1) maintenance action required if no logbook complaint. EIS II Software SXT3CE2SA0420 SXT4EE2SA050A TBD Associated P/N : DU PFD FO(1WK2)/ PFD FO POT(7WK2) maintenance action required if no logbook complaint. EIS II Software SXT3CE2SA0420 SXT4EE2SA050A TBD Associated P/N : DU SD(2WK2)/ECP(2WM) maintenance action required if no logbook complaint. EIS II Software SXT3CE2SA0420 SXT4EE2SA050A TBD Associated P/N : Part A : page 19

29 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref AFS:CHK DMCi-FMGCj CKT (i=1 or 2) (j=1 or 2) NO MAINT. ACTION required if no log book complaint FMGC ALL P/N TBD Filter Associated P/N : HUDC : CHECK DMC1 NO MAINT. ACTION HUDC TFU Associated P/N : HUDC : NO DMC1 D NO MAINT. ACTION HUDC TFU Associated P/N : CHECK LGCIU-PHC3 NO MAINT. ACTION if triggered in FWC flight phase 06 or 07 and if not associated with fault message "L/G EXT PROX SNSR 24GA(25GA) TGT POS" BSCU E E TBD Associated P/N : LGCIUi 05GAi NO MAINT. ACTION LGCIU A4A A4B TFU Associated P/N : Part A : page 20

30 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref SDACi:NO D FROM BSCU SDACi:NO D FROM BSCU1 (I=1 or 2) Wrong REF. Should be instead. All FWC in BASIC configuration (Pre Mod 24159) are affected (E2, E3, E4, F2). Wrong REF. Should be instead. All FWC in BASIC configuration (Pre Mod 24159) are affected (E2, E3, E4, F2) BSCU(10GG) NO MAINT. ACTION if the associated TSD shows fault code 530 AND if triggered on ground during Engine start or Engine shut-down AND A/C equipped with BSCS EMM (mod 26925). FWC FWC 350E E E E053020x0x (x=3, 4, 6) Associated P/N : 350E E E E053020x0x (x=3, 4, 6) Associated P/N : BSCU E TBD FWC STD H2F3 (Target: Oct 2005) FWC STD H2F3 (Target: Oct 2005) Filter Associated P/N : SDAC : NO D FROM BSCU NO MAINT. ACTION if no Log Book complaint SDAC 35-0E E E Associated P/N : SDAC : NO D FROM TPIU NO MAINT. ACTION if no Log Book complaint SDAC 35-0E E E Associated P/N : Part A : page 21

31 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref ABCU(95GG)/ BRK SELECTOR VALVE(23GG) NO MAINT. ACTION if triggered in flight phase 01 or 02 on A/C equipped with BSCS EMM (mod 26925) BSCU E TBD Filter Associated P/N : SDACi: LH Y BRK PRESS XDCR 63GG. (i=1 OR 2) A) NO MAINT ACTION if the fault message occurs in phase 06 and is not associated with the fault message "BRK ALTN PRESS TRANSDUCER 101GG" Source BSCU. B)Wrong FIN number coded in FWC BITE message. Should be 101GG instead. FWC 350E (FWC H2F2) FWC H2F3 P/N TBD Associated P/N : BSCU Post MOD SDACi:RH Y BRK PRESS XDCR 62GG. (i=1 OR 2) A) NO MAINT ACTION if the fault message occurs in phase 06 and is not associated with the fault message "BRK ALTN PRESS TRANSDUCER 100GG" Source BSCU. B) Wrong FIN number coded in FWC BITE message. Should be 100GG instead. FWC 350E (FWC H2F2) FWC H2F3 P/N TBD Associated P/N : BSCU Post MOD STEERING ELECTRO HYDRAULIC MODULE 6GC MAINT. ACTION if fault message triggered after Landing Gear free fall extension and code 58 (code 6A on A320 with BOGIE) has been recorded in BSCU BITE. BSCU C SERIES C SERIES N/A Associated P/N : PRE MOD STEERING ELECTRO-HYD MODULE (6GC) MAINT. ACTION if fault message triggered after Landing Gear free fall extension and code 654 has been recorded in BSCU BITE. BSCU E21327 SERIES N/A Associated P/N : PRE MOD Part A : page 22

32 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref AOA SENSOR 3FP1(2,3) Associated with the ECAM warning ANTI ICE CAPT (F/O,STBY) AOA. PHC TFU / TFU / TSM 30 Filter Associated P/N : AOA SNSRi (3FPi)/ ADIRUi(1FPi) NO MAINTENANCE ACTION if appears after an AOA test. ADIRU TFU Associated P/N : ADIRU1+3 (1FP1+3) BUS IR/WXR1 (1SQ1) If no logbook complaint, do not remove the RTA-4B from the aircraft. Power cycling the RTA-4B or executing the Radar Test on the MCDU will clear the nuisance fault if it continues to be displayed in Ground Scanning. RTA-4B ADIRUi+3(1FPi+3) ADRBUS /WXRi(1SQi) (i = 1 or 2) Associated P/N : maintenance action required if no logbook complaint. RADAR Associated P/N : AFS:ADIRU 1/2/3 DISAGREE NO MAINT. ACTION if not associated to any Message in the ADIRU Bite FAC B397AAM0507/0508 B397BAM0509 B397BAM0406/0407 B397AAM0509 B397CAM0101 TFU Associated P/N : Part A : page 23

33 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref AFS:ADIRU 1/2/3 DISAGREE NO MAINT.ACTION IF NO LOGBOOK COMPLAINT. Pitot Pre SB SB TFU (Pitot re-location) Filter Associated P/N : AFS:ADIRU 1/2/3 DISAGREE maintenance action if no logbook complaint FAC B397AAM0507 B397AAM0508 B397BAM0406 B397BAM0407 B397BAM0513 TFU Associated P/N : NO ADIRUi D CHECK WIRING TO SLT(FLP)i When this message is followed by SFCC1(2), 21(22)CV ignore this second message. SFCC TFU QUALIFIER Di/WXRj (1SQj) (i=1 or 2 and j= 1 or 2) Associated P/N : maintenance action if no logbook compaint. RADAR Associated P/N : RADARi: NO D FROM ADIRU The fault appears during ground test. Repeat test. If result OK no further MAINT ACTION required. RADAR SIL Rev.1 Associated P/N : Part A : page 24

34 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref RADARi:NO D FROM ADIRU NO MAINT. ACTION if no log book complaint RADAR VSB WRT-701X VSB WRT-701X Filter Associated P/N : HUD OHU NO MAINT. ACTION if no log book complaint. HUDC V65 SOFTWARE TFU AFS : ILS i NO MAINT. ACTION if occurs at the end of the flight FMGC All P/N Associated P/N : TBD FWCi :NO D FROM ILSi Associated P/N : NO MAINT ACTION if occurs in flight phases 02 and 07. ILS Associated P/N : ILS i RECEIVER NO MAINT. ACTION if no Log book complaint ILS TFU Associated P/N : Part A : page 25

35 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref ILSi NO MAINT. ACTION if occurs in flight phase 02. ILS NONE Filter ILSi (2RTi) NO MAINT. ACTION required if no logbook complaint. When receiver not tuned to any station, a self test is performed and this spurious message may be triggered. Associated P/N : ILS Collins VSB ILS ILS Associated P/N : MMR1 (40RT1)/GPWC (1WZ) NO MAINT. ACTION required EGPWS ILSi RECEIVER Ref TSM task associated to ILS fault " ILSi RECEIVER" Associated P/N : ILS NO MLS (i) D maintenance action if no logbook complaint AMU 3514xS01 Associated P/N : TBD Associated P/N : Part A : page 26

36 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref RADAR 1 ANTENNA NO MAINT. ACTION if no log book complaint RADAR VSB WRT-701X VSB WRT-701X Filter Associated P/N : RADAR i ANTENNA NO MAINT ACTION if nologbook complaint RADAR VSB RTA-4A Rev.1 TFU Associated P/N : RADAR i ANTENNA NO MAINT ACTION if message recorded immediately after engine start (this item concerns only 2 airlines) RADAR MI TBD NONE Associated P/N : WXR ANTENNA(11SQ) maintenance action required if no logbook complaint. RADAR Associated P/N : RADAR 1 CONTROL UNIT NO MAINT. ACTION if no log book complaint RADAR VSB WRT-701X VSB WRT-701X Associated P/N : Part A : page 27

37 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref WXR CTL PNL(3SQ)/ WXRi(1SQi) (i = 1 or 2) NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect. RADAR Filter DMCi: NO WXRj CHj D (i=1, 2 or 3; j=1 or 2) Associated to ECAM warning "NAV PRED W/S DET FAULT". Perform AMM Task "EIS Input TEST". If test ok, the WXR/DMC interface works properly and the WXR transceiver units should not be removed. If the test fails, apply corresponding TSM procedure x "Loss of Weather Radar Channel j bus identified by the EIS i". Associated P/N : RADAR Associated P/N : RADAR 1 TRANSCEIVER NO MAINT. ACTION if no log book complaint RADAR TBD VSB WRT-701X VSB WRT-701X Associated P/N : RADAR i TRANSCEIVER NO MAINT ACTION if message recorded immediately after engine start (this item concerns only 2 airlines). RADAR MI TBD NONE Associated P/N : RADARi TRANSCEIVER NO MAINT. ACTION if no log book complaint RADAR VSB RTA-4A Rev.1 TFU Associated P/N : Part A : page 28

38 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref WXRi(1SQi) (i=1 or 2) Maint. Action if fault msg recorded in the PFR without cockpit effect and is associated with specific TSD (final 4 digits "0000"). The fault msg may be triggered if radar selected OFF and Pred Windshear scanning automatically activated during take-off or approach. RADAR Filter WXRi(1SQi) (i= 1 or 2) Associated P/N : maintenance action if no logbook complaint. RADAR WXR MOUNTING TRAY(5SQ)/ WXRi(1SQi) (i = 1 or 2) Associated P/N : maintenance action required if no logbook complaint. RADAR Associated P/N : RA1 (2SA1) +RA2 (2SA2) / WXR1 (1SQ1) If no logbook complaint, do not remove the RTA-4B from the aircraft. Power cycling the RTA-4B or executing the Radar Test on the MCDU will clear the nuisance fault if it continues to be displayed in Ground Scanning. RADAR Associated P/N : RA1(2SA1)+RA2((2SA2)/ WXRi (1SQi) (I=1 or 2) NO MAINT. ACTION if recorded during Engine Start (flight phase 02) or during switching from WXR1 to WXR2 and no associated cockpit effect. RADAR Associated P/N : Part A : page 29

39 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref DMC(i): NO TCAS D (i = 1 or 2) maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS ACSS TBD TFU Filter Associated P/N : DMC(i): NO TCAS D (i = 1 or 2) maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS HONEY WELL x x / TBD TFU Associated P/N : DMC(i): NO TCAS D (i = 1 or 2) maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS ROCKW ELL TBD TFU TCAS ARINC 429 NO MAINT ACTION if no logbook complaint. This deviation has been identified. Associated P/N : TCAS TFU Associated P/N : TCAS UNTRACEABLE NO MAINT ACTION if no log book TCAS complaint. TCAS TFU Associated P/N : Part A : page 30

40 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref FWC(i): NO D FROM TCAS (i = 1 or 2) FWC(i): NO D FROM TCAS (i = 1 or 2) maintenance action required if no logbook complaint and if TCAS BITE is OK. maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS HONEY WELL TCAS ACSS x x / Associated P/N : TBD TFU TBD TFU Filter Associated P/N : FWC(i): NO D FROM TCAS (i = 1 or 2) maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS ROCKW ELL TBD TFU NO TCAS D maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS ROCKW ELL Associated P/N : TBD TFU Associated P/N : NO TCAS D maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS ACSS TBD TFU Associated P/N : Part A : page 31

41 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref NO TCAS D maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS ROCKW ELL TBD TFU Filter Associated P/N : NO TCAS D maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS HONEY WELL x x / TBD TFU Associated P/N : NO TCAS D maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS ACSS TBD TFU Associated P/N : ATC(i): NO D FROM TCAS (i = 1 or 2) maintenance action required if associated to the TCAS fault message " TCAS (1SG)" and if TCAS BITE is OK. TCAS TPA-81A REV2 TPA-81A TPA-81A REV1 TFU Associated P/N : ATC(i): NO D FROM TCAS (i = 1 or 2) maintenance action if no logbook complaint and if TCAS BITE is OK. TCAS ROCKW ELL TBD TFU Associated P/N : Part A : page 32

42 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref ATC(i): NO D FROM TCAS (i = 1 or 2) ATC(i): NO D FROM TCAS (i = 1 or 2) maintenance action if no logbook complaint and if TCAS BITE is OK. maintenance action if no logbook complaint and if TCAS BITE is OK. TCAS HONEY WELL TCAS ACSS x x / Associated P/N : TBD TFU TBD TFU Filter Associated P/N : TCAS (1SG) maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS TPA-81A REV2 TPA-81A TPA-81A REV1 TFU TCAS(1SG) maintenance action required if no logbook complaint and if TCAS BITE is OK TCAS(1SG) maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS HONEY WELL TCAS ROCKW ELL Associated P/N : x x / Associated P/N : TBD TFU TBD TFU Associated P/N : Part A : page 33

43 SIL PART A : Failure Messages Failure message Remark Part P/Ns Affected Corrective P/N Doc X Ref TCAS(1SG) maintenance action required if no logbook complaint and if TCAS BITE is OK. TCAS ACSS TBD TFU Filter Associated P/N : MODE S i NO MAINT ACTION if no logbook complaint. TCAS TFU AFS:DMEi NO MAINT ACTION if no log book complaint FMGC PEGASU S Associated P/N : C13042xA01 TBD Associated P/N : AFS:DMEi Due to A/C out of emitter range. Maint. Action if no Log Book complaint. DME VSB DME VSB DME TFU DME i TRANSCEIVER NO MAINT. ACTION if no log book complaints DME Associated P/N : B398BxM0xxx FMGC LEGACY VSB DME TFU Associated P/N : Part A : page 34