1EFF : ALL 1 22-92-00Page 7 1 1 May 01/05 1 1 1CES 1
C. List of FMGC/FM Error Codes
---------------------------------
R ------------------| EVENT | EVENT |
R | NO | | RESANA | NUMBER | DESIGNATION |
R |SYMETRY| SYMETRY| RESANAC |--------|----------------------|
R ----------|-------|--------| RESANAM |1 |LRU TEST |
R | | | | ---------|2 |185 HARDWARE FAIL |
R | | | |<---|.|.|.|.|--->|3 |IOP HARDWARE FAIL |
R | | | | |-|-|-|-| |4 |SOFTWARE FAIL |
R | | | | | | |5 |LRU FAIL |
R |---------|-------|--------| (ERROR CODE) |6 |FM POWER UP |
R |7 |DUAL FAIL |
R |--------|----------------------|
---------------------------------------------------------
| ERROR CODE | DESIGNATION |
|-------------|-----------------------------------------|
| 01 to 0F | NONE |
|-------------|-----------------------------------------|
| 10 to 11 | NONE |
| 12 | ADC OPP FAIL |
| 13 | ADC 3 FAIL |
| 14 TO 1D | NONE |
| 1E | ADC OWN FAIL |
| 1F | IRS OWN FAIL |
|-------------|-----------------------------------------|
| 20 to 2B | NONE |
| 2C | DME OPP FAIL |
| 2D | VOR OPP FAIL |
| 2E | ILS OPP FAIL |
| 2F | IRS OPP FAIL |
|-------------|-----------------------------------------|
| 30 | NONE |
| 31 | FAC OPP FAIL |
| 32 | FADEC OPP FAIL |
| 33 | MCDU OPP FAIL |
| 34 TO 37 | NONE |
| 38 | FM/FG POWER UP FAIL |
| 39 | MEMORY MODULE MISMATCH |
| 3A | MEMORY MODULE REMOVED |
| 3B | NAV DATA BASE MISMATCH |
| 3C | PROGRAM PIN MISMATCH |
| 3D | RESYNCH HAS OCCURED |
| 3E | NONE |
| 3F | IRS 3 FAIL |
|-------------|-----------------------------------------|
1EFF : ALL 1 22-92-00Page 8 1 1 Nov 01/04 1 1 1CES 1 ---------------------------------------------------------| ERROR CODE | DESIGNATION | |-------------|-----------------------------------------| | 40 to 4C | NONE | | 4D | FMGC OPP FAIL | | 4E to 4F | NONE | |-------------|-----------------------------------------| | 50 | FCU FAIL | | 51 TO 5F | NONE | |-------------|-----------------------------------------| | 60 | ACARS OPP FAIL | | 61 | RESYNCH HAS FAILED | | 62 | 185 HARDWARE FAIL | | 63 | IOP HARWARE FAIL | | 64 | SOFTWARE FAIL | | 65 | DME OWN FAIL | | 66 | VOR OWN FAIL | | 67 | ILS OWN FAIL | | 68 | CLOCK FAIL | | 69 | FAC OWN FAIL | | 6A | FADEC OWN FAIL | | 6B | FQI FAIL | | 6C | MCDU OWN FAIL | | 6D | ACARS OWN FAIL | | 6E | PRINTER FAIL | | 6F | DATA LOADER FAIL | |-------------|-----------------------------------------| | 70 to 74 | NONE | | 75 | LRU TEST PASS | | 76 | LRU TEST FAIL | | 77 to 7F | NONE | |-------------|-----------------------------------------| | F3 | NONE | |-------------|-----------------------------------------|
1EFF : ALL 1 22-92-00Page 9 1 1 Feb 01/98 1 1 1CES 1
AFS TEST (AFTER AFS LRU REMOVAL) - DESCRIPTION AND OPERATION
____________________________________________________________
1. General
_______ The purpose of the AFS TEST is to check the integrity of the AFS after replacement of an LRU (line replaceable unit). The AFS TEST completes the AFS computer monitoring and safety tests. This test, which is performed in the FACs and the FMGCs (FM and FG sections) consists in:
-using the computer safety test results (FAC, FG, FM, FCU and MCDU)
-
the test of symmetrical discrete inputs : FAC COM and FAC MON, FG COM and MON
-
the test of the symmetrical ARINC inputs
-
the plausibility test of the information delivered by:
-
the RUD TRIM/RESET pushbutton switch
-
the rudder trim control switch
-Capt A/THR instinctive disconnect pushbutton switch
-F/O A/THR instinctive disconnect pushbutton switch
-Capt takeover and priority pushbutton switch
-F/O takeover and priority pushbutton switch
-FAC engagement pushbutton switch.
2. Triggering of the AFS TEST
__________________________
On the ground in menu mode by selecting the AFS TEST option.
1EFF : ALL 1 22-96-00Page 1 1 1 Feb 01/98 1 1 1CES 1 3. Execution of the AFS TEST in the FIDS
_____________________________________ The test request is sent by the FIDS (fault isolation and detection system) to the various FAC, FG and FM BITEs. In order to prevent unwanted triggering of the test in flight, these BITEs only accept the request if their ground condition is met (NOSE GEAR PRSD).
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