Loss of the Bleed Regulated-Pressure Transducer of the Engine 2

TASK 36-11-00-810-820-A
Loss of the Bleed Regulated-Pressure Transducer of the Engine 2

1. Possible Causes

wiring between pin A/1 of the bleed regulated-pressure transducer (8HA2) and the circuit breaker (2HA2)
wiring between pin A/2 of the bleed regulated-pressure transducer (8HA2) and the ground terminal
XDCR-BLEED REGULATED PRESS, ENG 2 [8HA2]
wiring from the bleed regulated-pressure transducer (8HA2) pins A/3 and A/4 to the BMC2 (1HA2) pins AA/12B and AA/11B
C/B-AIR BLEED/ENG 2/MONG [2HA2]

2. Job Set-up Information
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 36-11-16-000-001	Removal of the Bleed Regulated Pressure-Transducer
AMM 36-11-16-400-001	Installation of the Bleed Regulated Pressure-Transducer

3. Fault Confirmation
Subtask 36-11-00-710-072-A ** ON A/C NOT FOR ALL

A. Test.
(1) Not applicable, the fault is evident.

4. Fault Isolation
Subtask 36-11-00-865-054-A ** ON A/C NOT FOR ALL

A. Table of the circuit breakers used in this procedure:

PANEL	DESIGNATION	FIN	LOCATION
** ON A/C NOT FOR ALL
122VU	AIR BLEED/ENG 2/MONG	2HA2	Z22

Subtask 36-11-00-810-061-A ** ON A/C NOT FOR ALL

B. If the fault symptom is identified by the maintenance message:
REG-PRESS XDCR 8HA2

(1) If the circuit breaker is closed

Do a check for 28VDC at pin A/1 of the bleed regulated-pressure transducer (8HA2) ASM 361102.

(a) If there is no 28VDC

Do a check of the wiring between pin A/1 of the bleed regulated-pressure transducer (8HA2) and the circuit breaker (2HA2).

1 If there is no continuity:

2 If there is continuity:

(b) If there is 28VDC:

Do a check for ground at pin A/2 of the bleed regulated-pressure transducer (8HA2).

1 If there is no ground:

Repair the wiring between pin A/2 of the bleed regulated-pressure transducer (8HA2) and the ground terminal.

2 If there is ground:

Replace the XDCR-BLEED REGULATED PRESS, ENG 2 [8HA2] AMM 36-11-16-000-001 and AMM 36-11-16-400-001.

a If the fault continues:

Do a check and repair the wiring from the bleed regulated-pressure transducer (8HA2) pins A/3 and A/4 to the BMC2 (1HA2) pins AA/12B and AA/11B ASM 361102

(2) If the circuit breaker is open:

(a) If the fault continues:

Subtask 36-11-00-710-073-A ** ON A/C NOT FOR ALL

C. After the subsequent flight, make sure that the fault does not continue.

[Rev.8 from Aug 2018] 2026.04.04 04:33:42 UTC