Load-Control Valve (P12) Fault (131-9(A))
TASK 49-00-81-810-861-A
Load-Control Valve (P12) Fault (131-9(A))
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 49-00-81-710-072-B ** ON A/C NOT FOR ALL
Subtask 49-00-81-810-064-K ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:40:38 UTC
Load-Control Valve (P12) Fault (131-9(A))
1. Possible Causes
- LOAD CONTROL VALVE SHOWS OPEN SWITCH FAILURE
- LOAD CONTROL VALVE SHOWS CLOSED SWITCH FAILURE
- LOAD VALVE SOLENOID SHOWS CIRCUIT FAILURE
- LOAD VALVE OPEN SIGNAL SHOWS CIRCUIT FAILURE
- LOAD CONTROL VALVE SHOWS NOT CLOSED
- LOAD CONTROL VALVE SHOWS OPEN AND CLOSED
- LOAD CONTROL VALVE SHOWS NOT OPEN
damage/contamination of electrical connector P12 LOAD CONTROL VLV (8050KM) - aircraft wiring
- ELECTRONIC CONTROL BOX [59KD]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 49-00-00-860-008 | APU Start by External Power |
| AMM 49-51-51-000-004 | Removal of the Load Control Valve (131-9(A)) |
| AMM 49-51-51-400-004 | Installation of the Load Control Valve (131-9(A)) |
| ASM 496104 | |
| 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 49-00-81-710-072-B ** 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:
LOAD CONTROL VALVE SHOWS OPEN SWITCH FAILURE
or
LOAD CONTROL VALVE SHOWS CLOSED SWITCH FAILURE
or
LOAD VALVE SOLENOID SHOWS CIRCUIT FAILURE
or
LOAD VALVE OPEN SIGNAL SHOWS CIRCUIT FAILURE
(b) Push the TEST line key.
(5) If the MCDU menu shows
LOAD CONTROL VALVE SHOWS NOT CLOSED
or
LOAD CONTROL VALVE SHOWS OPEN AND CLOSED
(6) If the MCDU menu shows
LOAD CONTROL VALVE SHOWS NOT OPEN
(b) Get access to the APU GND SCANNING menu.
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:
LOAD CONTROL VALVE SHOWS OPEN SWITCH FAILURE
or
LOAD CONTROL VALVE SHOWS CLOSED SWITCH FAILURE
or
LOAD VALVE SOLENOID SHOWS CIRCUIT FAILURE
or
LOAD VALVE OPEN SIGNAL SHOWS CIRCUIT FAILURE
- do the Fault Confirmation that follows:
(b) Push the TEST line key.
(5) If the MCDU menu shows
LOAD CONTROL VALVE SHOWS NOT CLOSED
or
LOAD CONTROL VALVE SHOWS OPEN AND CLOSED
- do the Fault Confirmation that follows:
(6) If the MCDU menu shows
LOAD CONTROL VALVE SHOWS NOT OPEN
- do the Fault Confirmation that follows:
(b) Get access to the APU GND SCANNING menu.
Subtask 49-00-81-810-064-K ** ON A/C NOT FOR ALL
A. If the APU GND SCANNING menu gives the maintenance message:
LOAD CONTROL VALVE (8050KM)
associated with Fault Code Number (FCN) 88, 92, 93, 96, 97 or 127
or
WRG: LOAD VALVE OPEN SIGNAL
associated with Fault Code Number (FCN) 138
Subtask 49-00-81-710-073-A ** ON A/C NOT FOR ALL LOAD CONTROL VALVE (8050KM)
associated with Fault Code Number (FCN) 88, 92, 93, 96, 97 or 127
or
WRG: LOAD VALVE OPEN SIGNAL
associated with Fault Code Number (FCN) 138
- do a check for
damage/contamination of electrical connector P12 of the LOAD CONTROL VALVE (8050KM).
- do a repair/cleaning.
- replace the
LOAD CONTROL VLV (8050KM) AMM 49-51-51-000-004 and AMM 49-51-51-400-004.
- do a check and repair of the aircraft wiring from
the ECB (59KD) AB/F10,D7,D14 to the LOAD CONTROL VALVE (8050KM) P12/1,3,4
the LOAD CONTROL VALVE (8050KM) P12/2 to GND
ASM 496104.
- 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.