#quot#APU AVAIL#quot#- Signal Fault (131-9(A))
TASK 49-00-81-810-862-A
"APU AVAIL"- Signal Fault (131-9(A))
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 49-00-81-710-074-A ** ON A/C NOT FOR ALL
Subtask 49-00-81-810-065-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:34:36 UTC
"APU AVAIL"- Signal Fault (131-9(A))
1. Possible Causes
- APU AVAILABLE SHOWS CIRCUIT FAILURE
- BOARD-ANN LT TEST & INTFC [7LP]
- aircraft wiring
- ELECTRONIC CONTROL BOX [59KD]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 33-14-00-710-001 | Operational Test of the Lights |
| AMM 33-14-33-000-001 | Removal of the Annunciator-Light Test and Interface-Board |
| AMM 33-14-33-400-001 | Installation of the Annunciator-Light Test and Interface-Board |
| ASM 496101 | |
| AMM 49-61-34-000-003 | Removal of the Electronic Control Box (ECB) (131-9(A)) |
| AMM 49-61-34-400-003 | Installation of the Electronic Control Box (ECB) (131-9(A)) |
Subtask 49-00-81-710-074-A ** ON A/C NOT FOR ALL
A. Read-out of ECB Trouble-Shooting Data
(1) Put the APU MASTER SW to the ON position.
(2) Get access to the APU LAST LEG/PREVIOUS LEG report.
(3) Push the '>'-key adjacent to the related CFDS failure message.
(4) If the MCDU menu shows:
APU AVAILABLE SHOWS CIRCUIT FAILURE
4. Fault Isolation(1) Put the APU MASTER SW to the ON position.
(2) Get access to the APU LAST LEG/PREVIOUS LEG report.
(3) Push the '>'-key adjacent to the related CFDS failure message.
(4) If the MCDU menu shows:
APU AVAILABLE SHOWS CIRCUIT FAILURE
- do the Fault Confirmation that follows:
Subtask 49-00-81-810-065-A ** ON A/C NOT FOR ALL
A. If the APU GND SCANNING menu gives the maintenance message:
WRG: APU AVAILABLE
associated with Fault Code Number (FCN) 130
Subtask 49-00-81-710-075-A ** ON A/C NOT FOR ALL WRG: APU AVAILABLE
associated with Fault Code Number (FCN) 130
- do the Operational Test of the Annunciator Light Test System in the Cockpit AMM 33-14-00-710-001.
- replace the BOARD-ANN LT TEST & INTFC [7LP] AMM 33-14-33-000-001 and AMM 33-14-33-400-001.
- replace the APU START P/B (2KA).
- do a check and repair of the aircraft wiring from the ECB (59KD) AB/J6 to
the RELAY-APU AVAIL (6KD) A/X1
and
the RELAY-ANNUNCIATOR-LIGHT TEST AND INTERFACE-BOARD (7LP) A/21 ASM 496101.
- replace the ELECTRONIC CONTROL BOX [59KD] AMM 49-61-34-000-003 and AMM 49-61-34-400-003.
B. Do the test given in Para. 3.