W DOC AIRBUS | TSM A320F

Engine 2 Bleed Temperature Sensor Channel A Measurement Failure


TASK 36-11-00-810-A06-A
Engine 2 Bleed Temperature Sensor Channel A Measurement Failure


1. Possible Causes
  • SENSOR-EXCHANGER OUT TEMP, ENG 2 [6HA2]
  • wiring
  • BMC-2 [1HA2]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ASM 361102
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 36-11-00-710-462-A ** ON A/C NOT FOR ALL
A. Test.
   (1) Not Applicable
4. Fault Isolation
Subtask 36-11-00-810-413-A ** ON A/C NOT FOR ALL
A. If the fault symptom is identified by the maintenance message:
TEMP SENSOR (6HA2)/BMC2 (1HA2)
Subtask 36-11-00-810-432-A ** ON A/C NOT FOR ALL
B. If the fault continues:
   (1) Do a check for ground for Exchanger Outlet Temperature-Sensor (6HA2) at pin G/2 of the BMC2 (1HA2).
     (a) If there is no ground:
       1 Do a check of the wiring from BMC2 (1HA2) pin G/2 and the ground terminal ASM 361102.
       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 (6HA2) pin A/1 and A/2 to BMC2 (1HA2) pin AA/2C and AA/2B ASM 361102.
       2 If you find damage in the wiring:
         a Repair or replace the wiring .
Subtask 36-11-00-810-419-A ** ON A/C NOT FOR ALL
C. If the fault continues:
Subtask 36-11-00-710-463-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