10V Pressure Reference not Correct (131-9(A))
TASK 49-00-81-810-899-A
10V Pressure Reference not Correct (131-9(A))
1. Possible Causes
A. Fixtures, Tools, Test and Support Equipment
B. Referenced Information
3. Fault Confirmation
Subtask 49-00-81-710-248-A ** ON A/C NOT FOR ALL
Subtask 49-00-81-810-164-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:34:39 UTC
10V Pressure Reference not Correct (131-9(A))
1. Possible Causes
- PRESS XDCR WIRING SHOWS OPEN CIRCUIT
APU INLET PRESSURE TRANSDUCER (P22) TOTAL PRESSURE TRANSDUCER (P23) DELTA PRESSURE TRANSDUCER (P24) - APU [4005KM]
- aircraft wiring
APU INLET PRESSURE TRANSDUCER (8048KM) TOTAL PRESSURE TRANSDUCER (8044KM) DELTA PRESSURE TRANSDUCER (8043KM)
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | MULTIMETER - STANDARD |
| REFERENCE | DESIGNATION |
|---|---|
| AMM 49-11-11-000-004 | Removal of the Power Plant (APU) (131-9(A)) |
| AMM 49-11-11-400-004 | Installation of the Power Plant (APU) (131-9(A)) |
| AMM 49-51-16-000-002 | Removal of the Transducer - Differential Pressure (131-9(A)) |
| AMM 49-51-16-400-002 | Installation of the Transducer - Differential Pressure (131-9(A)) |
| AMM 49-51-17-000-002 | Removal of the Transducer - Total Pressure (131-9(A)) |
| AMM 49-51-17-400-002 | Installation of the Transducer - Total Pressure (131-9(A)) |
| AMM 49-51-21-000-001 | Removal of the Transducer - APU Inlet Pressure (131-9(A)) |
| AMM 49-51-21-400-001 | Installation of the Transducer - APU Inlet Pressure (131-9(A)) |
| ASM 496104 |
Subtask 49-00-81-710-248-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 '>' adjacent to the related CFDS failure message:
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 '>' adjacent to the related CFDS failure message:
- the MCDU menu shows
PRESS XDCR WIRING SHOWS OPEN CIRCUIT
Subtask 49-00-81-810-164-A ** ON A/C NOT FOR ALL
A. If the APU GND SCANNING menu gives the maintenance message:
CHECK PRESSURE XDCR WIRING
associated with Fault Code Number (FCN) 30
Subtask 49-00-81-810-164-B ** ON A/C NOT FOR ALL CHECK PRESSURE XDCR WIRING
associated with Fault Code Number (FCN) 30
- disconnect the electrical connector P2 at the APU firewall.
Use a MULTIMETER - STANDARD to do a resistance check across pin 20 and pin 21 of the electrical connector P2.
- disconnect the electrical connector P22 of the APU INLET PRESSURE TRANSDUCER (P22).
Do a resistance check across pin 20 and pin 21 of the electrical connector P2 again.
- replace the
APU INLET PRESSURE TRANSDUCER (P22) AMM 49-51-21-000-001 and AMM 49-51-21-400-001.
- disconnect the electrical connector P23 of the TOTAL PRESSURE TRANSDUCER (P23).
Do a resistance check across pin 20 and pin 21 of the electrical connector P2 again.
- replace the
TOTAL PRESSURE TRANSDUCER (P23) AMM 49-51-17-000-002 and AMM 49-51-17-400-002.
- disconnect the electrical connector P24 of the DELTA PRESSURE TRANSDUCER (P24).
Do a resistance check across pin 20 and pin 21 of the electrical connector P2 again.
- replace the
DELTA PRESSURE TRANSDUCER (P24) AMM 49-51-16-000-002 and AMM 49-51-16-400-002.
- replace the APU [4005KM] AMM 49-11-11-000-004 and AMM 49-11-11-400-004.
- do a check and repair of the aircraft wiring between ECB (59KD) AB/A1,A4 and electrical connector P2/20,21 ASM 496104.
A. If the APU GND SCANNING menu gives the maintenance message:
CHECK PRESSURE XDCR WIRING (8001KM)
associated with Fault Code Number (FCN) 30
Subtask 49-00-81-710-249-A ** ON A/C NOT FOR ALL CHECK PRESSURE XDCR WIRING (8001KM)
associated with Fault Code Number (FCN) 30
- disconnect the electrical connector P2 at the APU firewall.
Use a MULTIMETER - STANDARD to do a resistance check across pin 20 and pin 21 of the electrical connector P2.
- disconnect the electrical connector P22 of the APU INLET PRESSURE TRANSDUCER (8048KM).
Do a resistance check across pin 20 and pin 21 of the electrical connector P2 again.
- replace the
APU INLET PRESSURE TRANSDUCER (8048KM) AMM 49-51-21-000-001 and AMM 49-51-21-400-001.
- disconnect the electrical connector P23 of the TOTAL PRESSURE TRANSDUCER (8044KM).
Do a resistance check across pin 20 and pin 21 of the electrical connector P2 again.
- replace the
TOTAL PRESSURE TRANSDUCER (8044KM) AMM 49-51-17-000-002 and AMM 49-51-17-400-002.
- disconnect the electrical connector P24 of the DELTA PRESSURE TRANSDUCER (8043KM).
Do a resistance check across pin 20 and pin 21 of the electrical connector P2 again.
- replace the
DELTA PRESSURE TRANSDUCER (8043KM) AMM 49-51-16-000-002 and AMM 49-51-16-400-002.
- replace the APU [4005KM] AMM 49-11-11-000-004 and AMM 49-11-11-400-004.
- do a check and repair of the aircraft wiring between ECB (59KD) AB/A1,A4 and electrical connector P2/20,21 ASM 496104.
B. Do a check of the APU GND SCANNING menu to verify the fault is not present.