Loss of the Bleed Transferred-Pressure Transducer of the Engine 2
TASK 36-11-00-810-818-A
Loss of the Bleed Transferred-Pressure Transducer of the Engine 2
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 36-11-00-710-068-A ** ON A/C NOT FOR ALL
Subtask 36-11-00-865-052-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:33:42 UTC
Loss of the Bleed Transferred-Pressure Transducer of the Engine 2
1. Possible Causes
wiring between pin A/2 of the bleed transferred-pressure transducer (7HA2) and the ground terminal wiring between pin A/1 of the bleed transferred-pressure transducer (7HA2) and the circuit breaker (2HA2) - XDCR-BLEED TRANSFER PRESS, ENG 2 [7HA2]
wiring from the bleed transferred-pressure transducer (7HA2) to the BMC2 (1HA2) - C/B-AIR BLEED/ENG 2/MONG [2HA2]
- BMC-2 [1HA2]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| TSM TASK 24-00-00-810-803-A | Circuit Breaker Tripped and/or C/B TRIPPED Warning |
| ASM 361102 | |
| AMM 36-11-15-000-001 | Removal of the Bleed Transferred Pressure-Transducer |
| AMM 36-11-15-400-001 | Installation of the Bleed Transferred Pressure-Transducer |
Subtask 36-11-00-710-068-A ** ON A/C NOT FOR ALL
A. Not applicable.
4. Fault IsolationSubtask 36-11-00-865-052-A ** ON A/C NOT FOR ALL
A. Table of the circuit breakers used in this procedure:
Subtask 36-11-00-810-059-A ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 122VU | AIR BLEED/ENG 2/MONG | 2HA2 | Z22 |
B. If the fault symptom is identified by the maintenance message TRANSF-PRESS XDCR 7HA2:
Subtask 36-11-00-810-059-B ** ON A/C NOT FOR ALL - Do a check of the status of the circuit breaker (2HA2).
- Do a check for 28VDC at pin A/1 of the bleed transferred-pressure transducer (7HA2) ASM 361102.
- Do a check for ground at pin A/2 of the bleed transferred-pressure transducer (7HA2).
- Repair the
wiring between pin A/2 of the bleed transferred-pressure transducer (7HA2) and the ground terminal .
- Do a check of the
wiring between pin A/1 of the bleed transferred-pressure transducer (7HA2) and the circuit breaker (2HA2)
- Repair the above wiring.
- Replace the circuit breaker (2HA2).
- Make sure that there is a 0 psig output signal (0.9VDC) on the BMC2 (1HA2) connector between pins AA/14A and AA/15B.
- Replace the XDCR-BLEED TRANSFER PRESS, ENG 2 [7HA2] AMM 36-11-15-000-001 and AMM 36-11-15-400-001.
- Do a check and repair the
wiring from the bleed transferred-pressure transducer (7HA2) to the BMC2 (1HA2) , pins A/3 and A/4 to pins AA/15B and AA/14B.
- Replace the XDCR-BLEED TRANSFER PRESS, ENG 2 [7HA2] .
- Do the procedure (Ref. TSM TASK 24-00-00-810-803).
- Replace the C/B-AIR BLEED/ENG 2/MONG [2HA2] .
- Replace the BMC-2 [1HA2] .
B. If the fault symptom is identified by the Class 3 maintenance message:
36-11-15
DRIFT TRANSF-PRESS XDCR 7HA2
Subtask 36-11-00-710-069-A ** ON A/C NOT FOR ALL 36-11-15
DRIFT TRANSF-PRESS XDCR 7HA2
- Do a check of the status of the circuit breaker (2HA2).
- Do a check for 28VDC at pin A/1 of the bleed transferred-pressure transducer (7HA2) ASM 361102.
- Do a check for ground at pin A/2 of the bleed transferred-pressure transducer (7HA2).
- Repair the
wiring between pin A/2 of the bleed transferred-pressure transducer (7HA2) and the ground terminal .
- Do a check of the
wiring between pin A/1 of the bleed transferred-pressure transducer (7HA2) and the circuit breaker (2HA2) .
- Repair the above wiring.
- Replace the circuit breaker (2HA2).
- Make sure that there is a 0 psig output signal (0.9VDC) on the BMC2 (1HA2) connector between pins AA/14A and AA/15B.
- Replace the XDCR-BLEED TRANSFER PRESS, ENG 2 [7HA2] AMM 36-11-15-000-001 and AMM 36-11-15-400-001.
- Do a check and repair the
wiring from the bleed transferred-pressure transducer (7HA2) to the BMC2 (1HA2) , pins A/3 and A/4 to pins AA/15B and AA/14B.
- Replace the XDCR-BLEED TRANSFER PRESS, ENG 2 [7HA2] .
- Do the procedure (Ref. TSM TASK 24-00-00-810-803).
- Replace the C/B-AIR BLEED/ENG 2/MONG [2HA2] .
- Replace the BMC-2 [1HA2] .
C. After the subsequent flight, make sure that the fault does not continue.