1AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 > AVS aboard ATR -600 Maintenance Function Thales Avionics 4 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 Centralized Maintenance Introduction » Maintenance includes CMF and BITE functions » CMF has two Modes Normal Mode Interactive Mode » CMF sub-functions Maintenance and configuration data processing Interactive tests and specific actions CFM NVM storage Correlation General parameters providing Interactions with operator and MCDU pages displaying AVS alarms transmission to MPC CAC #1 CMF is mainly realized by the CMA SW application that operates only in CAC1 5 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 BITE Function Purpose and Architecture BITE Function » Ensures concentration and processing of sub-system maintenance data from continuous monitoring (CBIT) and automatic test at power on (ABIT), and provides these data to the CMF » And also, according to sub-system, gives more information about failures (failure context) in order to help shop maintenance teams. » Includes the set of BITE functions implemented in each AVS sub-system: COTS Sub-systems having BITE function with pre-determined functionalities, Non COTS Sub-systems having specific functionalities in the AVS context (IAD, CAC) Non-COTS sub-system BITE Function of COTS CMF BITE Function of non-COTS APPLI n COTS sub-system 6 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 BITE Function Modes and Interfaces » The BITE function operates Normal mode Interactive mode (processing of interactive requests from CMF) » Sub-functions and modes Interfaces with » CMF according to the sub-system type (1 or 2) the BITE function of COTS and Non- COTS sub-systems exchanges Maintenance data, General parameters, if needed, Interactive commands. » Avionics application Maintenance data with their associated context Interactive commands, if needed » Programming pins BITE function of non COTS LRU acquires their side/position through Programming pins, and use, by default side 1, if acquisition failed Ident. Sub-Function Normal Mode Interactive Mode F01 CBIT reporting X - F02 Test and Specific actions - X F03 BITE function NVM storage X X F04 General parameters acquisition X X F05 LRU identification data transmission X X 7 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 Failures Classification and Sub-System Types Failure Class » Class 1 Failure leading to a flight deck effect (highest class) » Class 2 Minor failures without flight deck effects (lowest class). Those failures require deferred maintenance Notes An external failure is a failure present on a LRU input Any CMF failure that induces a lost of redundancy is defined as a Class 1 failure Sub-System Types » Type 1 with one A429 numeric bus in input and one A429 numeric bus output HF1, HF2, VHF1 NAV, VHF2 NAV, DME1, DME2, VHF COM1, VHF COM2, VHF COM3, DU1, DU2, DU3, DU4, DU5, CAC1, CAC2, CMU, ATC » Type 2 with one discrete input and one A429 numeric bus output IRS1, IRS2, ADU1, ADU2, AHRS1, AHRS2 ARINC bus ARINC bus Unit C M F ARINC bus Unit C M F 8 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 Maintenance Messages and Architecture » Access to CMA via A429 VHF COMVDL2, T2CAS, RA, CMU, ATC XPDR, ADU, IRS, AHRS, VHF NAV, VHF NAV&ADF, MCDU » Access to CMA via AFDX VHF COM, HF COM, DME, GPS, CPM CBITE, IAD, WXR 9 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - Transmission of Maintenance Data - via DU Case 1 Case 2 Case 3 Case 4 10 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - Transmission of Maintenance Data - via CAC Transmission of Maintenance Data - from CAC2 LRU FGCP, ICP1 ,ICP2, CPSTN1, CPSTN2, CPSTN3, SM1, SM2, SM3, PTB1, PTB2, IOM-AP1, IOM-AP2, IOM-DC11, IOM-DC12, IOM-DC21, IOM-DC22, IOM-S1, IOM-S2 Appli AFA, DCA, CSW 11 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - Types of Messages » Bit Oriented Format (BOF) For A429 A set of bits where each failure is coded by using one or n bits transmitted by 1 or n A429 words » Basic Failure Message (BFM) For AFDX A set of bits where each failure is coded by using one or n bits transmitted by 1 or n Functional Data Set of AFDX message Bit Location Bit Description 8 - 1 Label (octal) 10 - 9 SDI, MSB = 10, LSB = 9 29 - 11 Failures indication (some bits may be not used according to sub-system) 31 - 30 SSM MSB = 31, SSM LSB = 30 32 Odd Parity Field Name Size Format Functional Block ID 4 Integer Vendor ID 4 Integer BITE Event Type 4 Integer BITE EVENT ID 4 Integer Info 1 4 Integer Info 2 4 Integer Info 3 4 Integer BITE Event State 4 Integer Sanction 4 Integer Engineering Data Length 4 Integer Engineering Data 0 - 83 Table of Bytes 12 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF Purpose and Architecture Centralized Maintenance Function » Ensures the concentration and processing of AVS maintenance data received from BITE function, and makes them available to the Operator via reports displayed on MCDU pages. » Offers to the maintenance Operator a set of services via MCDU pages in order to make a diagnostic that permits to identify most clearly possible root cause of a problem occurrence in AVS, such as: Display of configuration report Display failures reports (current failures and historical), Possibility to initiate interactive tests Note: CMF displays its MCDU pages via MPC (out of AVS). BITE Function n Date, Time, A/C configuration, Flight ground conditions MPC Maintenance data General parameters Interactive commands MCDU pages CMF MCDU#1 MCDU pages BITE Function 2 BITE Function 1 MCDU#2 13 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF Modes CMF Normal mode Power cut or re-initialization or ending of interactive mode by the operator or Maintenance phase become “Flight” or default in communication between the MCDU and the CMF. Power-up CMF Interactive mode Maintenance phase is "Ground" and action of the operator on a dedicated key from Maintenance MCDU pages Power cut or re-initialization CMF is in normal mode by default 14 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF External Interfaces » Interface with MPC for MCDU CMF exchanges data with the MCDU (requests/responses from protocol + MCDU pages) via MPC CMF communicates with MPC in A739 that manages the communication with MCDU » Interface for Clock CMF acquires Date, Time (in this order) from CLOCK1, or CLOCK2 in case of failure, or FMS1 in case of failure, or then FMS2 in case of failure CMA1 receives from • DCA1 date, time from CLOCK1 • DCA2 date, time from CLOCK2 • FMS1 date, time • FMS2 date, time » Flight phase acquisition CMF acquires flight phase from MPC » Peripheral availability acquisition CMF acquires periodically peripheral availability label from MPC Printer and PCMCIA disk » Interface for Avionic options and A/C configuration CMF acquires AVS configuration file from FDA » Programming pins CMF acquires Programming Pins from CPM1 and CPM2 » Date and Time Stamping CMF provides general parameters (Date, Time, A/C Identification, Maintenance command to Type 1 sub-systems 15 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 Typical Scenario When the A/C is on Ground phase, the maintenance Operator consults failures reports in order to isolate the failure. » Failures messages accuse clearly a LRU The Operator launches an interactive test on the sub-system containing the LRU to confirm the failure. Then, he consults its Trouble Shouting Manual (TSM) and Minimum Equipment List (MEL), and applies the maintenance procedure related to the LRU identified as failed. In case this procedure recommends to change the LRU, the maintenance Operator He removes / replaces the accused LRU, Verifies the good operation by using current failures report or interactive test from the CMF. » Failure messages accuse a link between several LRU The Operator consults its database of maintenance procedures (out of CMF scope) and applies the usual procedure related to a problem of link. » Failures messages indicate more than one possibility The maintenance Operator has to complete the diagnostic by his own means. He may use current failures report of the CMF to verify if each operation performed has an effect on the problem. When the diagnostic is ended and the problem isolated the maintenance Operator conducts the relevant maintenance tasks. 16 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - Functional and Performance Data » CFM NVM storage CMF stores failures detected in flight (filtered with the appropriated correlation and configuration), and needed data reported from AVS in Non Volatile Memory (NVM) non-erasable » PREVIOUS LEGS REPORT CMF stores in NVM up to 300 class 1 failures that occurred during the previous 63 legs, the oldest failures being replaced by the newest ones » LAST LEG REPORT CMF stores in NVM up to 50 class 1 of the last leg failures by applying the following rules - The possibility is offered to store at least one message for each subsystem - The oldest failures being replaced by the newest ones » LAST LEG REPORT At the start of a new leg, all the messages from last leg are transferred in the previous legs zone of the NVM to allow their display in the PREVIOUS LEGS REPORT menu. » MAINT REPORT CMF stores in NVM up to 300 class 2 failures occurred during the 64 last legs by applying the following rules - The possibility is offer to store at least one message for each subsystem in a leg - The oldest failures being replaced by the newest ones » No fault redundancy in a leg The detection of a system failure which is identical to a most recent failure logged in NVM is not repeated in the same leg. 17 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - Maintenance and Flight Phases Failures Storage criteria When maintenance command is DC2, only internal failures are stored in NVM When maintenance command is DC1 internal failures and external failures are stored in NVM When no valid Flight Phase available, Maint. Phase = Flight, Maint. Command = DC1 Pre Flight 1 Taxi out 2 TO init. roll initial 3 TO final roll final 4 Initial climb 5 Flight Phase 6 Final App. 7 LDG roll 8 Taxi In 9 Post Flight 10 Flight phase Pre Flight 1 +1 Leg count Last leg Leg Previous leg Ground Ground Flight Maintenance phase +30 S NULL DC1 Maintenance command 30 S min DC2 NULL 18 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - MCDU Pages AVIONICS STATUS LRU IDENT SUB-SYST n TESTS SUB-SYST n AVS MAIN MENU PROMPT « AVS » LRU IDENT SUB-SYST n LAST LEG REPORT SUB-SYST n PREVIOUS LEGS REPORT SUB-SYST n MAINT SUB-SYST n LAST LEG REPORT PREVIOUS LEGS REPORT AVS AND A/C OPT CONF SYS REPORT / TEST SUB-SYST LIST LRU IDENT SUB- SYST LIST TEST RESULTS MAINT SUB-SYST n MAIN MENU 19 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 MCDU General Presentation LSK L1 LSK L2 LSK L3 LSK L4 LSK L5 LSK L6 LSK R1 LSK R2 LSK R3 LSK R4 LSK R5 LSK R6 LSK R1 AVS < AVIONICS STATUS < LAST LEG REPORT < RETURN SYSTEM > REPORT / TEST < PREVIOUS LEGS REPORT MAINT > LRU IDENT > AVS AND A/C > OPT CONF PRINT * Example of CMF MCDU Main Menu 20 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - AVIONICS STATUS REPORT description » AVIONICS STATUS Faulty LRU are ordered Class 1 first and alphabetically CONF_UPDATED_MESSAGEs in first, and then failed LRUs, and at last other error messages When during 5 seconds, there is no data or invalid data received by CMF from an avionic LRU, CMF displays "NO DATA FROM LRU i" or "INVALID DATA FROM LRU i“ The displayed pages are not automatically refreshed AVIONICS STATUS 1/N CONF_UPDATED _MESSAGE <LRUx X > NO POWER SUPPLY FROM BUSBARx <NO DATA FROM sub-system y CLASS < < < < < < > > > > > > < RETURN <INVALID DATA FROM sub-system z PRINT * AVIONICS STATUS NO FAULT REPORTED < < < < < < > > > > > > < RETURN PRINT * Case of failure recorded No fault recorded 21 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - LAST LEG REPORT Description » LAST LEG Displays Class 1 failures from AVS stored in NVM and occurred during the last leg when maintenance phase was "Flight“ The date and the time of the failure are the first failure occurrence date and first detection time of the failure The ATA code of failure is the code of the highest suspect LRU The most recent failure messages is listed first LAST LEG REPORT 1/N MESSAGE 1 > TIME MAR 05 1910 MESSAGE 2 > ATA 31-50-00 DATE > > > > > > < < < < < < < RETURN PRINT * MAR 05 1902 34-00-00 SUB-SYSTEM NAME < LAST LEG REPORT < PREVIOUS LEGS REPORT < SYSTEM TEST / SPECIFIC ACTION < MAINT > > > > > > < < < < < < < RETURN < LRU IDENT PRINT * LAST LEG REPORT NO FAULT REPORTED > > > > > > or 22 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - PREVIOUS LEG REPORT Description » PREVIOUS LEG Displays Class 1 failures from AVS stored in NVM and occurred during the previous 63 legs when maintenance phase was "Flight“ Only the failures that have occurred on the same A/C (same A/C Identification) are reported on a same page The first displayed failure is the most recent failure of the most recent leg Use PREV key to display the oldest flight At the start of a new leg • The flight leg number of PREVIOUS LEG REPORT is incremented, and • The leg 64 (if it exists) deleted from NVM PREV LEGS REPORT 1/N LEG MESSAGE 1 TIME MAR 10 1910 MESSAGE 2 MAR 05 1902 ATA 31-50-00 34-00-00 A/C IDENT DATE 01 02 > > > > > > < < < < < < < RETURN PRINT * NO FAULT REPORTED PREV LEGS REPORT > > > > > > < < < < < < < RETURN PRINT * LEG 00 Last Leg LEG 01 First previous leg LEG 02 Previous leg preceding LEG 01 … … 23 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description » SYSTEM REPORT / TEST Displays the list of all sub-systems names managed by CMF An action on the LSK associated with a prompt lets the Operator enter the main menu of the relevant sub-system If the sub-system is not fitted on the A/C (see AVS configuration file), the information NOT FITTED is displayed on the line following the name of the sub- system, and the prompt sign in front of the LRU removed. Note: If the Operator uses the corresponding line key, the menu currently displayed does not change Navigation by means of keys SYSTEM REPORT/TEST 1/4 < RETURN < CAC1 < CAC2 < MCDU1 < MCDU2 < DU1 DU2 > DU3 > DU4 > DU5 > CMU > PRINT * SYSTEM REPORT/TEST 2/4 < RETURN < HF1 < HF2 < VHF COM1 < VHF COM2 < VHF COM3 VHF NAV&ADF1 > VHF NAV2 > DME1 > DME2 > GPS1 > PRINT * PREV … NEXT SYSTEM REPORT/TEST 3/4 < RETURN < GPS2 < RA1 < RA2 < WXR < XPDR1/ T2CAS XPDR2/T2CAS > ADC1 > ADC2 > AHRS1 > AHRS2 > PRINT * SYSTEM REPORT/TEST 4/4 < RETURN < IRS1 < IRS2 PRINT * < AFCS 24 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description (Cont’d) » SYSTEM REPORT / TEST Type 1 / 2 systems main menu When no SYSTEM TEST and no SPECIFIC ACTION then line associated to third key is empty, when no LRU IDENT available for the system then line associated to fifth key is empty Note: AHRS implements a specific action: flux valve calibration » LAST LEG REPORT for Type 1/ 2 system Displays only failure messages related to the selected sub-system contained in LAST LEG REPORT of all AVS SUB-SYSTEM NAME < LAST LEG REPORT < PREVIOUS LEGS REPORT < SYSTEM TEST / SPECIFIC ACTION < MAINT > > > > > > < < < < < < < RETURN < LRU IDENT PRINT * 1/N MESSAGE 1 TIME MAR 05 1910 MESSAGE 2 MAR 05 1902 ATA 31-50-00 34-00-00 DATE SUB-SYSTEM NAME LAST LEG REPORT > > > > > > < < < < < < < RETURN PRINT * SUB-SYSTEM NAME LAST LEG REPORT NO FAULT REPORTED > > > > > > or 25 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description (Cont’d) » PREVIOUS LEG REPORT for Type 1 / 2 system Displays only Class 1 failure messages related to the selected sub-system contained in PREVIOUS LEGS REPORT of all AVS SUB-SYSTEM NAME < LAST LEG REPORT < PREVIOUS LEGS REPORT < SYSTEM TEST / SPECIFIC ACTION < MAINT > > > > > > < < < < < < < RETURN < LRU IDENT PRINT * SUB-SYSTEM NAME LAST LEG REPORT NO FAULT REPORTED > > > > > > or PREV LEGS REPORT A/C IDENT 1/N MESSAGE 1 TIME MAR 05 1910 MESSAGE 2 MAR 05 1902 ATA 31-50-00 34-00-00 DATE SUB-SYSTEM NAME > > > > > > < < < < < < LEG 01 02 < RETURN PRINT * 26 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description (Cont’d) » SYSTEM TEST for maintenance / functional / self test of Type 1 / 2 system SUB-SYSTEM NAME SYSTEM TEST / SPECIF ACT If test ended and failures reported If test ended and No Failure reported < START SELF-TEST > > > > > > < < < < < < SUB-SYSTEM NAME < LAST LEG REPORT < PREVIOUS LEGS REPORT < SYSTEM TEST / SPECIFIC ACTION < MAINT > > > > > > < < < < < < < START PUSH-TO-TEST < RETURN < RETURN If (test initiated (with command or discrete) and no pre-condition SUB-SYSTEM NAME SELF-TEST > > > > > > < < < < < < < LRU IDENT PRINT * PRINT * PRINT * > > > > > > < < < < < < PRINT * If pre-condition CANCEL > CONTINUE > SUB-SYSTEM NAME SELF-TEST 31-32-00 MESSAGE 1 34-42-01 MESSAGE 2 > > > > > > < < < < < < < RETURN CLASS 1 2 ATA PRINT * SUB-SYSTEM NAME SELF-TEST TEST IN PROGRESS 90 SECONDS MAX TEST Pre-condition ERROR TEST ABORTED > > < < SUB-SYSTEM NAME SELF-TEST TEST OK > > < < SUB-SYSTEM NAME SELF-TEST If No label received during 4 seconds or unit status is failed and no failures or test inhibited or unit not in test after 5 sec or Timeout 27 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description (Cont’d) » SYSTEM TEST for maintenance / functional / self test of Type 1 / 2 system When a UNIT test Pre-Condition required CMA1 displays PULL CB: UNIT Name WAIT 5S, THEN PUSH CB UNIT Name PRESS CONTINUE OR CANCEL With UNIT Name ACARS CMU, VHF COM3, GPS, WXR, CAPT DU1 PFD, CAPT DU2 MFD, DU3 EWD, F/O DU4 MFD, F/O DU5 PFD, CAPT MCDU, F/O MCDU » LRU state after Initiated test from Maintenance Function After an Initiated Test (IBIT, push to test) the system is in the same state as before the initiated Test, with the same Pre selected data Displays Mode selection 28 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 » SYSTEM TEST for HF COM and Self-test is activated CMF - SYSTEM REPORT / TEST Description (Cont’d) HF COM SELF TEST If test ended with failure reported < START SELF-TEST > > > > > > < < < < < < HF COM < LAST LEG REPORT < PREVIOUS LEGS REPORT < SYSTEM TEST / SPECIFIC ACTION < MAINT > > > > > > < < < < < < < RETURN < RETURN 31-32-00 MESSAGE 1 34-42-01 MESSAGE 2 (1) If No label received during 4 seconds or unit status is failed and no failures or unit not in test after 5 sec or test inhibited or Timeout Test requested > > > > > > < < < < < < < RETURN > > > > > > < < < < < < < RETURN HF COM RECEIVE SELF-TEST TEST IN PROGRESS 60 SECONDS MAX > > > > > > < < < < < < < LRU IDENT CLASS 1 2 ATA PRINT * PRINT * PRINT * PRINT * PRINT * <START TRANSMIT TEST < START TRANSMIT TEST HF COM RECEIVE SELF-TEST HF COM RECEIVE SELF-TEST ERROR TEST ABORTED > > < < TEST OK HF COM RECEIVE SELF-TEST If test ended and No Failure reported 29 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 » SYSTEM TEST for HF COM and Transmit-test is activated (Cont’d) CMF - SYSTEM REPORT / TEST Description (Cont’d) (1) If test ended and Failures reported If test ended and No Failure reported 31-32-00 MESSAGE 1 34-42-01 MESSAGE 2 TEST OK > > > > > > < < < < < < < RETURN 1/N > > > > > > < < < < < < < RETURN CLASS 1 2 ATA PRINT * PRINT * HF COM TRANSMIT SELF-TEST Pre-condition > > > > > > < < < < < < PRINT * CANCEL > CONTINUE > ERROR TEST ABORTED > > > > > > < < < < < < < RETURN test requested TEST IN PROGRESS 60 SECONDS MAX > > > > > > < < < < < < PRINT * PRINT * from previous slide If No label received during 4 seconds or unit status is failed and no failures or test inhibited or unit not in test after 5 sec or Timeout HF COM TRANSMIT SELF-TEST HF COM TRANSMIT SELF-TEST HF COM TRANSMIT SELF-TEST HF COM TRANSMIT SELF-TEST NOTE: During HFCOM self-test, CMA1 displays the pre-conditions in the dedicated MCDU page: CAUTION: HF WILL EMIT INSURE SAFETY REF JIC 231100 OPT 10000 KEEP PTT HF PRESSED AND AT THE SAME TIME PRESS CONTINUE KEY 30 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description (Cont’d) CACx SYSTEM TEST < START SELF-TEST > > < < If test of CPM1 CANCEL > CPM1 SELF-TEST > > > > > > < < < < < < PULL CB CAC1 CPM IOM S WAIT FOR 5 SECONDS SET IN CB COM WITH MCDU WILL BE LOST PRINT * PULL CB CAC2 CPM IOM S WAIT FOR 5 SECONDS SET IN CB PRESS CONTINUE CPM2 SELF-TEST > > > > > > < < < < < < If test of CPM2 CANCEL > CONTINUE > PRINT * CACx < LAST LEG REPORT < PREVIOUS LEGS REPORT < SYSTEM TEST / SPECIFIC ACTION < MAINT > > > > > > < < < < < < < RETURN < LRU IDENT PRINT * TEST IN PROGRESS 60 SECONDS MAX CACx TEST NAME » SYSTEM TEST for CPM If Test in progress CACx TEST NAME ERROR TEST ABORTED CACx TEST NAME TEST OK CACx TEST NAME 31-32-00 MESSAGE 1 34-42-01 MESSAGE 2 1/N > > > > > > < < < < < < < RETURN CLASS 1 2 ATA PRINT * If test ended and Failures reported If test ended and No Failure reported If data from CPM BITE invalid or Timeout or No Data during 5s 31 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description (Cont’d) » SYSTEM TEST for AFCS AFCS SYSTEM TESTS < START CPM1 SELF-TEST > > > > > > < < < < < < < RETURN PRINT * < START CPM2 SELF-TEST < START AFCS TEST AFCS POST AFCS POST IN PROGRESS 60 SECONDS MAX > > > > > > < < < < < < PRINT * If TEST ABORTED message received from AFCA1 or TEST REQ ACK timeout TEST ABORTED > > > > > > < < < < < < < RETURN PRINT * 27-32-33 MESSAGE 1 42-11-84 MESSAGE 2 TEST OK > > > > > > < < < < < < < RETURN 1/N > > > > > > < < < < < < < RETURN CLASS 1 1 ATA PRINT * PRINT * CONTINUE > CONTINUE > AFCS POST AFCS POST AFCS POST If test ended and Failures reported If AFCA ABIT ended and No Failure reported (1) 32 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description (Cont’d) » SYSTEM TEST for AFCS (Cont’d) CONTINUE > If AFCA motion ended and Failures reported If AFCA motion ended and No Failure reported 27-32-33 MESSAGE 1 42-11-84 MESSAGE 2 If TEST ABORTED message received from AFCA1 or TEST REQ ACK timeout TEST OK > > > > > > < < < < < < < RETURN > > > > > > < < < < < < < RETURN CLASS 1 1 ATA PRINT * PRINT * AFCS MOTION CAUTION: CTRL SURFACES WILL MOVE INSURE SAFETY IF EMERGENCY: USE QUICK RELEASE REF JIC 221800 OPT 10000 > > > > > > < < < < < < < RETURN PRINT * TEST ABORTED > > > > > > < < < < < < < RETURN TEST IN PROGRESS 120 SECONDS MAX > > > > > > < < < < < < PRINT * PRINT * (1) AFCS MOTION AFCS MOTION AFCS MOTION AFCS MOTION Note In AFCS test result of AFCS POST or AFCS motion, CMA displays only failures detected by AFCA 33 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description (Cont’d) » SYSTEM TEST for PUSH-TO-TEST of Type 1 / 2 system SUB-SYSTEM NAME SYSTEM TEST < START PUSH-TO-TEST > > > > > > < < < < < < SUB-SYSTEM NAME < LAST LEG REPORT < PREVIOUS LEGS REPORT < SYSTEM TEST / SPECIFIC ACTION < MAINT > > > > > > < < < < < < < RETURN < RETURN SUB-SYSTEM NAME PUSH TO TEST IN PROGRESS SYSTEM TEST > > > > > > < < < < < < < STOP < LRU IDENT < START SELF-TEST Note The line START SELF TEST is not displayed if the sub-system doesn’t implement self-test PRINT * PRINT * PRINT * CMA1 permits to start One self-test for each CPM, VHF COM, VHF COM VDL2 (VHF COM3), VHF NAV, HF COM, DME, IRS, ADU, AHRS, ATC (XPDR) / T2CAS (ATC test induces also T2CAS test), MCDU, CMU, RA, GPS, WXR, DU One VOR-ILS self-test and one ADF self-test for VHF NAV&ADF One push-to-test for ADU If test can't be executed, CMA1 displays on the last line (line 14) "SYSTEM NOT AVAILABLE" in case of no response or sub-system already in test "SYSTEM ERROR" in case of sub-system bad response returned by sub-system or no computed data received from sub- system (except for VHCOM1/2 or 3 for which Non Computed Data does not imply the display of "SYSTEM ERROR") 34 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description (Cont’d) In the particular case of MCDU, if MCDUi is used for displaying maintenance information, MCDUi test is inhibited in the corresponding menu » SYSTEM TEST for MCDU MCDU MCDUi USED FOR CMF DISPLAY : TEST INHIBITED PLEASE USE THE OTHER MCDU TO TEST THIS ONE > > > > > > < < < < < < < RETURN PRINT * 35 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description (Cont’d) AHRSx SYST TEST/ SPECIF ACT < START SELF-TEST > > > > > > < < < < < < AHRSx < LAST LEG REPORT < PREVIOUS LEGS REPORT < SYSTEM TEST / SPECIFIC ACTION < MAINT > > > > > > < < < < < < < RETURN < RETURN < LRU IDENT < FLUX VALVE CALIBRATION Notes x (from AHRSx) is replaced par the side of the current AHRS y (from AHRSy) is replaced by the side of opposite AHRS val1: heading value in degree (decimal resolution 0.1) val2, val3: equal to 1 or 0 VALIDATE: when pressed, the heading tuned with Right Heading and Left Heading, key is validated Upon selection of “GO TO AHRSy” key CMA permits to access to the page containing “CAL MODE” key of the opposite AHRS not in calibration mode “HDG+ / HDG-“ of the opposite AHRS already in calibration mode AHRSx <CAL MODE FLUX VALVE CALIBRATION > > > > > > < < < < < < PRESS CAL MODE key DURING 3s TO SET AHRSx CALIBRATION MODE < RETURN PRINT * PRINT * PRINT * CAL MODE key pressed during 3s END CALIB key pressed during 3s <HDG - > > > > > > < < < < < < HEADING: val1 VHDG: val2 VALIGN: val3 HDG + > <VALIDATE <END CALIB GO TO AHRSy > QUIT: press 3s END CALIB PRINT * AHRSx FLUX VALVE CALIBRATION During tuning, if no response from AHRS is received by CMF within 5 seconds about Heading, Heading degradation, Alignment in progress, the message SYSTEM NOT AVAILABLE appears on the last line (line 14). » SYSTEM TEST for AHRS 36 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description (Cont’d) For the Type 1 and 2 sub-systems, pressing MAINT report from a sub-system main menu displays only Class 2 failures related to the selected sub-system contained in MAINT report of all AVS » SYSTEM TEST for MAINT Report Failures transmitted No failure transmitted MAINT REPORT NO FAULT REPORTED SUB-SYSTEM NAME > > > > > > < < < < < < < RETURN 1/N MESSAGE 1 TIME MAR 05 1910 MESSAGE 2 MAR 05 1902 ATA 31-50-00 34-00-00 DATE SUB-SYSTEM NAME MAINT REPORT A/C IDENT > > > > > > < < < < < < LEG 01 02 < RETURN SUB-SYSTEM NAME < LAST LEG REPORT < PREVIOUS LEGS REPORT < SYSTEM TEST / SPECIFIC ACTION < MAINT > > > > > > < < < < < < < RETURN < LRU IDENT PRINT * PRINT * PRINT * 37 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - SYSTEM REPORT / TEST Description (Cont’d) For loadable sub-systems, pressing LRU IDENT report from a sub-system main menu displays LRU IDENT report containing part number of the sub- system » SYSTEM TEST for LRU IDENT Report If more than one LRU SUB-SYSTEM NAME < LAST LEG REPORT < PREVIOUS LEGS REPORT < SYSTEM TEST < MAINT > > > > > > < < < < < < < RETURN < LRU IDENT LRU1 IDENT 1/N LRUn (FINn): : HW P/N: XXXXXXXXXXXX P/N3:XXXXXXXXXXXX < < < < < < < RETURN P/N1:XXXXXXXXXXXX P/N2:XXXXXXXXXXXX LRUn CPMn (for CACn) or DUn or SWMn HW P/N Harware Part Number P/Nn Part Number of loadable (Software, Database, Configuration File) FINn FIN code of the LRUn Subsystem Name CACn or DUn or SWMn P/N4:XXXXXXXXXXXX P/N5:XXXXXXXXXXXX P/N6:XXXXXXXXXXXX P/N7:XXXXXXXXXXXX PRINT * PRINT * Note: The only sub-system that have more than one LRU with LRU ident to display is CACx, the two LRU are CPMx and SWMx (x=1 or 2) SUB-SYSTEM NAME 1/1 < LRU1 < LRU2 > > > > > > < < < < < < < RETURN PRINT * < LRUn < < < < < < If one LRU 38 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - MAINT REPORT Description » MAINT report displays Class 2 failures from AVS stored in NVM and occurred during the 64 last legs when maintenance phase was "Flight" (failures without effect on system operation) » In MAINT REPORT a leg shall contain at the maximum 50 failures MAINT REPORT NO FAULT REPORTED No failure recorded Failures recorded > > > > > > < < < < < < < RETURN MAINT REPORT A/C IDENT 1/N MESSAGE 1 TIME MAR 05 1910 MESSAGE 2 MAR 05 1902 ATA 31-50-00 34-00-00 DATE > > > > > > < < < < < < LEG 00 01 < RETURN AVS < AVIONICS STATUS < LAST LEG REPORT > > > > > > < < < < < < < RETURN SYSTEM > REPORT / TEST < PREVIOUS LEGS REPORT MAINT > LRU IDENT > AVS AND A/C > OPT CONF PRINT * PRINT * PRINT * 39 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - LRU IDENT Description from CAC » When a LRU type is selected, the CMF displays the part number transmitted by each side the selected LRU type » LRU IDENT report lets the Operator display the Part Number of CAC-CPM (loadable on A/C) LRU IDENT < CAC < DU > > > > > > < < < < < < < RETURN PRINT * AVS < AVIONICS STATUS < LAST LEG REPORT > > > > > > < < < < < < < RETURN SYSTEM > REPORT / TEST < PREVIOUS LEGS REPORT MAINT > LRU IDENT > AVS AND A/C > OPT CONF PRINT * CPM LRU IDENT 1/2 > > > > > > < < < < < < < RETURN PRINT * CPM1 HW:XXXXXXXXXXXX CMA SW:XXXXXXXXXXXX AFCA SW:XXXXXXXXXXXX FWA SW:XXXXXXXXXXXX CMA SW:XXXXXXXXXXXX DCA SW:XXXXXXXXXXXX DCA SW:XXXXXXXXXXXX CPM2 HW:XXXXXXXXXXXX AFCA SW:XXXXXXXXXXXX FWA SW:XXXXXXXXXXXX CPM LRU IDENT 2/2 > > > > > > < < < < < < < RETURN PRINT * CPM1 CSW:XXXXXXXXXXXX MCCT:XXXXXXXXXXXX MCCT:XXXXXXXXXXXX CPM2 CSW:XXXXXXXXXXXX FWMCF:XXXXXXXXXXXX MNTCF:XXXXXXXXXXXX MNTCF:XXXXXXXXXXXX FWMCF:XXXXXXXXXXXX SUB-SYSTEM NAME < CPM <SWM > > > > > > < < < < < < < RETURN PRINT * PREV … NEXT 40 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - LRU IDENT Description from CAC (Cont’d) » When a LRU type is selected, the CMF displays the part number transmitted by each side the selected LRU type » LRU IDENT report lets the Operator display the Part Number of CAC-SWM (loadable on A/C) LRU IDENT < CAC < DU > > > > > > < < < < < < < RETURN PRINT * AVS < AVIONICS STATUS < LAST LEG REPORT > > > > > > < < < < < < < RETURN SYSTEM > REPORT / TEST < PREVIOUS LEGS REPORT MAINT > LRU IDENT > AVS AND A/C > OPT CONF PRINT * SUB-SYSTEM NAME < CPM <SWM > > > > > > < < < < < < < RETURN PRINT * SWM LRU IDENT > > > > > > < < < < < < < RETURN PRINT * SWM1 HW:XXXXXXXXXXXX CSW:XXXXXXXXXXXX CF : XXXXXXXXXXXX SWM2 HW:XXXXXXXXXXXX CF : XXXXXXXXXXXX CSW:XXXXXXXXXXXX 41 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - LRU IDENT Description from DU » When a LRU type is selected, the CMF displays the part number transmitted by each side the selected LRU type » LRU IDENT report lets the Operator display the Part Number of DU (loadable on A/C) LRU IDENT < CAC < DU > > > > > > < < < < < < < RETURN PRINT * AVS < AVIONICS STATUS < LAST LEG REPORT < < < < < < < RETURN SYSTEM > REPORT / TEST < PREVIOUS LEGS REPORT MAINT > LRU IDENT > AVS AND A/C > OPT CONF PRINT * DU LRU IDENT 1/4 < RETURN PRINT * DU1 HW:XXXXXXXXXXXX IAD SW:XXXXXXXXXXXX DU2 HW:XXXXXXXXXXXX DU3 HW:XXXXXXXXXXXX DU4 HW:XXXXXXXXXXXX DU5 HW:XXXXXXXXXXXX IAD SW:XXXXXXXXXXXX IAD SW:XXXXXXXXXXXX IAD SW:XXXXXXXXXXXX IAD SW:XXXXXXXXXXXX z DU LRU IDENT 3/4 < RETURN PRINT * DU1 FMCF42:XXXXXXXXXXXX FMCF72:XXXXXXXXXXXX DU2 FMCF42:XXXXXXXXXXXX DU3 FMCF42:XXXXXXXXXXXX DU4 FMCF42:XXXXXXXXXXXX DU5 FMCF42:XXXXXXXXXXXX FMCF72:XXXXXXXXXXXX FMCF72:XXXXXXXXXXXX FMCF72:XXXXXXXXXXXX FMCF72:XXXXXXXXXXXX DU LRU IDENT 2/4 < RETURN PRINT * FMPDB72:XXXXXXXXXXXX DU2 FMPDB42:XXXXXXXXXXXX DU3 FMPDB42:XXXXXXXXXXXX DU4 FMPDB42:XXXXXXXXXXXX DU5 FMPDB42:XXXXXXXXXXXX FMPDB72:XXXXXXXXXXXX FMPDB72:XXXXXXXXXXXX FMPDB72:XXXXXXXXXXXX FMPDB72:XXXXXXXXXXXX DU1 FMPDB42:XXXXXXXXXXXX z DU LRU IDENT 4/4 < RETURN PRINT * DU1 AVSCF:XXXXXXXXXXXX DU2 AVSCF:XXXXXXXXXXXX DU3 AVSCF:XXXXXXXXXXXX DU4 AVSCF:XXXXXXXXXXXX DU5 AVSCF:XXXXXXXXXXXX PREV … NEXT > > > > > > 42 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - AVS and A/C OPT CONF Description The CMF displays all Avionic options and A/C configuration parameters from AVS configuration AVS < AVIONICS STATUS < LAST LEG REPORT < < < < < < < RETURN SYSTEM > REPORT / TEST < PREVIOUS LEGS REPORT MAINT > LRU IDENT > AVS AND A/C > OPT CONF PRINT * PREV … NEXT > > > > > > AVS AND A/C OPT CONF A/C SN : A/C_SN_Val HW PINPROG A/C TYPE CPM1: val1 A/C CAT CPM1: val2 A/C TYPE CPM2: val3 A/C CAT CPM2: val4 SW PINPROG A/C OPTIONS: A/C VIDEO: AC-video_val 1/5 < RETURN PRINT * AVS AND A/C OPT CONF 2/5 < RETURN AFT CARGO: AC_AFT_CARGO_val FWD CARGO: AC_FWD_CARGO_val PRES ALT: AC_PRES_ALT_val PROP_BRK_L: AC_PROP_BRK_L_val PROP_BRK_R: AC_PROP_BRK_R_val ENG RATING: AC_ENG_ val FLAP 25: AC_FLAP_val ENG BOOST: AC_ENG_BOOST_val FAA PROC : AC-FAA-PROC_val ST3 ST5: AVS_ST3_ST5_val PRINT * AVS AND A/C OPT CONF 3/5 < RETURN PRINT * ST6: AVS_ST6_val SW PINPROG AVS OPTIONS: ADF2: AVS_ADF2_val DME2: AVS_DME2_val GPS2: AVS_GPS2_val HF1: AVS_HF1_val HF2: AVS HF2_val RA2 : AVS_RA2_val AHRS/IRS: AVS_INERTIAL_val AVS AND A/C OPT CONF ACARS: AVS_DL1_val ADSB-IN: AVS-TCAS_val AIRPORT MAP: AVS_OANS_ val STEEP APP: AC_SteepAPP_val SPD HLD: AC_SPD_HLD_val WXR MODE: AVS-WXR1_val TAWS MODE AVS-WXR2_val CPLD VNAV: AVS-NAV1_val NAV TO NAV: AVS-NAV2_val SATCOM: AVS-SATCOM_ val 4/5 < RETURN PRINT * AVS AND A/C OPT CONF SATCOM/GSM: AVS-SATCOM2_val CPDLC: AVS-DL2_val GLS: AVS-GLS_val RNP SAAR: AVS-RNP_val VSD: AVS-VSD_val E-VSD: AVS-VSD2_val GBAAS: AVS-GBAAS_ val 5/5 < RETURN PRINT * Notes - val1 = ATR42 or ATR72 (CPM1 pinprog) - val2 = CATII or CATIII (CPM1 pin-prog) - val3 = ATR42 or ATR72 (CPM2 pinprog) - val4 = CATII or CATIII (CPM2 pinprog) - Other string ended by _val are replaced by the real string value contained in AVS configuration file - The length of value may be greater than one line, in this case next lines are moved downward - When data acquisition failed val are dashed 43 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - Maintenance Tips » Failure of special LRU AFCA failures include failures of CPSTN, SM, PTB, IOM-AP, FGCP, ICP DCA failures include failures of IOM-DC CPM PTF failures include failures of IOM-S FDA failures include failures of EFCP-L, EFCP-R, MCP » COTS detect All its internal failures (due to an internal problem inside LRU) All its external failures (failures on input interfaces only of sub-systems really fitted) Note: failures include hardware and software failures 44 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - Maintenance Tips - ABIT - CBIT » ABIT All LRU contain adequate ABIT, initiated automatically on power-up to verify CPU self-test Memory checksum (program and data memory) Test of peripheral circuits Test of I/O ports (complete wraparound test to detect the absence of emission) Note: ABIT (Automatic Build-In Test) = monitoring done at LRU initialization also called PBIT (Power on BIT) or POST (Power On Self-Test) » CBIT of non COTS Non COTS sub-systems perform CBIT during operation in order to verify fault-free system operation CPU fail, Memory fail, Peripheral fail, Watch dog, Applications failure, Interface failures » CBIT of COTS COTS sub-systems perform CBIT during operation in order to verify fault-free system operation CPU fail, Memory fail, Peripheral fail, Watch dog 45 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - Onboard SW Dataloading Dataloading allowed if 46 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - Sub-function DUMP BITE » Dump of IAD BITE IAD Dump Bite is performed with a dedicated CPF containing an identifier detected by the IAD on ground only Contents of the SBite memory is then copied in a dedicated folder on the CPF During the operation, the IAD displays a message and a progressive bar for the maintenance operator IAD BITE RECORDING IN PROGRESS IAD BITE RECORDING COMPLETED » Dump of CPM/IOM-S BITE Performed using the PMAT on ground A request of the content of the CPM SBite and CMA logbooks is performed Result of the operation is send to the gateway (for the PMAT) using a dedicated instrumentation VL 47 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 IAD CAC1 CMF - Dataloading General PC PMAT CD-ROM Load Ethernet Link CPF SW Upload Dump BITE CACPF IAD SW Upload Dump BITE PMAT = Thales Software + PC + Ethernet cable CPM & SWM CD-ROM IAD CD-ROM 48 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - Dataloading Order Acronym Designation Host Root Dataloading order CPM CSW Common Core Software CPM K4018 1 CPM CCT CPM Complete Configuration Table CPM G6041 2 AFCA Automatic Flight Control Application CPM G2865 3 FWA Flight Warning Application CPM G2867 3 FWCF Flight Warning Configuration File CPM G2868 4 DCA Data Concentration Application CPM G2875 3 CMA-BITE Centralized Maintenance Application - CPM Complete BITE CPM G2874 3 CM FT Centralized Maintenance Failure Table CPM G2912 4 SWM CSW Switch Module Core Software SWM K4045 1 NCT Network Configuration Table SWM G6042 2 49 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - Example of CPM Dataloading Procedure - Switch on the Laptop - Execute « PMAT Software» link - Enter the “User Name” and the “PWD” 50 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF - Example of Procedure for Upload IAD SW on a CPF - Switch on the Laptop - Execute « PMAT Software» link - Enter the “User Name” and the “PWD” - Power off IAD - Install the CPF with Operational SW in IAD - Power on IAD - A green “L” appears on IAD - At the end of loading, the green “L” becomes a white “L” if there was no uploading problem or a red “L” in case of uploading problem - If there was no uploading problem, then power off IAD - Remove CPF from the IAD - Power on IAD 51 AVS aboard ATR -600 GENFAM L&B Abb Quiz ? Avionics Services Worldwide Customer Training Centre > R e f . G E D : A S W / 1 1 / 0 0 1 4 7 6 CMF Transfer from Patrice to Trainees Now that’s time to practice. Be lazy and use your brain…