W DOC AIRBUS | TSM A320F

Engine 1 Bleed Temperature Sensor Channel A Measurement Failure


TASK 36-11-00-810-A04-A
Engine 1 Bleed Temperature Sensor Channel A Measurement Failure


1. Possible Causes
  • SENSOR-EXCHANGER OUT TEMP, ENG 1 [6HA1]
  • wiring
  • BMC-1 [1HA1]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
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 36-11-34-000-001
Removal of the BMC
AMM 36-11-34-400-001
Installation of the BMC
3. Fault Confirmation
Subtask 36-11-00-710-458-A ** ON A/C NOT FOR ALL
A. Test
   (1) Not Applicable
4. Fault Isolation
Subtask 36-11-00-810-411-A ** ON A/C NOT FOR ALL
A. If the fault symptom is identified by the maintenance message:
TEMP SENSOR (6HA1)/BMC1 (1HA1)
Subtask 36-11-00-810-454-A ** ON A/C NOT FOR ALL
B. If the fault continues:
   (1) Do a check for ground at Exchanger Outlet Temperature-Sensor (6HA1) pin G/1 of the BMC1 (1HA1).
     (a) If there is no ground:
       1 Do a check of the wiring from BMC1 (1HA1) pin G/1 and the ground terminal ASM 361101.
       2 If you find damage in the wiring:
         a Repair or replace the wiring
     (b) If there is ground:
       1 Do a check of the wiring from Exchanger Outlet Temperature-Sensor (6HA1) pin B/1 and B/2 to BMC1 (1HA1) pin AA/2C and AA/2B ASM 361101.
       2 If you find damage in the wiring:
         a Repair or replace the wiring
Subtask 36-11-00-810-455-A ** ON A/C NOT FOR ALL
C. If the fault continues:
   (1) Replace the BMC-1 [1HA1] AMM 36-11-34-000-001 and AMM 36-11-34-400-001.
Subtask 36-11-00-710-459-A ** ON A/C NOT FOR ALL
D. After the subsequent flight, make sure that the fault does not continue.
[Rev.8 from Aug 2018] 2026.04.04 04:33:55 UTC