Low Bleed Temperature of the Engine 1 in Climb

TASK 36-11-00-810-886-A
Low Bleed Temperature of the Engine 1 in Climb

1. Possible Causes

2. Job Set-up Information
A. Referenced Information

REFERENCE	DESIGNATION
AMM 36-11-00-740-001	BITE Test of the BMC 1(2)
ASM 361101
AMM 36-11-17-000-001	Removal of the Heat-Exchanger Outlet-Temperature Sensor
AMM 36-11-17-400-001	Installation of the Heat-Exchanger Outlet-Temperature Sensor
AMM 36-11-43-000-001	Removal of the Fan-Air Valve Control-Thermostat
AMM 36-11-43-400-001	Installation of the Fan-Air Valve Control-Thermostat
AMM 36-11-54-000-001	Removal of the Fan Air Valve
AMM 36-11-54-400-001	Installation of the Fan Air Valve

3. Fault Confirmation
Subtask 36-11-00-710-219-A ** ON A/C NOT FOR ALL

A. Test
(1) Do the BITE test of the BMC 1 AMM 36-11-00-740-001.

4. Fault Isolation
Subtask 36-11-00-810-136-A ** ON A/C NOT FOR ALL

A. If the fault symptom is identified by the class 3 maintenance message:
TEMP SENSOR 6HA1

Replace the SENSOR-EXCHANGER OUT TEMP, ENG 1 [6HA1] AMM 36-11-17-000-001 and AMM 36-11-17-400-001.

(1) If the fault continues:

Do a check of the wiring ASM 361101 between:
. pin 4 of the engine 1 exchanger output temperature sensor (6HA1) and pin AA/10B of the BMC 1 (1HA1)
. pin 2 of the engine 1 exchanger output temperature sensor and pin AA/9B of the BMC 1
. pin 1 and the ground.

(a) If the wiring is not correct:

(b) If the wiring is correct:

1 If the fault continues:

Replace the THERMOSTAT-FAN AIR VALVE CTL [7170HM] AMM 36-11-43-000-001 and AMM 36-11-43-400-001.

Subtask 36-11-00-710-220-A ** ON A/C NOT FOR ALL

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

[Rev.8 from Aug 2018] 2026.04.04 04:33:47 UTC