W DOC AIRBUS | TSM A320F

Pack 1 Outlet Temperature Sensor Fault


TASK 21-61-00-810-830-A
Pack 1 Outlet Temperature Sensor Fault


1. Possible Causes
  • SENSOR-PACK OUTLET TEMP [13HH]
  • wiring
  • P1 CHECK VALVE TRIM AIR [18HM]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 21-61-00-710-001
Operational Test of the Pack Temperature-Control System
ASM 216104
AMM 21-61-15-000-001
Removal of the Pack Outlet - Temperature Sensors
AMM 21-61-15-400-001
Installation of the Pack Outlet - Temperature Sensors
AMM 21-63-42-210-001
Detailed Visual Inspection of Trim-Air Check-Valves Flappers for Condition and Operation
3. Fault Confirmation
Subtask 21-61-00-710-108-A ** ON A/C NOT FOR ALL
A. Do the operational test of the pack temperature-control system AMM 21-61-00-710-001.
NOTE: If a fault is detected, the PC gives a fault code for shop maintenance in addition to the related CFDS message(s) (refer to TSM chapter 21-63-00, page block 301).
Subtask 21-61-00-710-108-B ** ON A/C NOT FOR ALL
A. Do the operational test of the pack temperature-control system AMM 21-61-00-710-001.
4. Fault Isolation
Subtask 21-61-00-810-122-A ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message P1 OUTLET TEMP SENSOR:
   (1) If the fault continues:
  • do a check and repair the wiring between:
    SENSOR (13HH) connector A/C and PC 1 (7HH) connector AB/12A,
    SENSOR (13HH) connector A/B and PC 1 (7HH) connector AB/12B,
    SENSOR (13HH) connector A/A and PC 1 (7HH) connector AB/11D ASM 216104.
   (2) If the fault continues:
  • do a visiual inspection of the trim-air check-valve flappers AMM 21-63-42-210-001 and replace this valve if nessesary.
Subtask 21-61-00-810-122-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message P1 OUT TEMP SENSOR(13HH):
   (1) If the fault continues:
  • do a check and repair the wiring ASM 216104 from:
  • the SENSOR (13HH) to the ACSC1 (47HH) and,
  • the SENSOR (13HH) to ground.
   (2) If the fault continues:
  • do a visual inspection of the P1 CHECK VALVE TRIM AIR [18HM] flappers AMM 21-63-42-210-001 and replace this valve if nessesary.
Subtask 21-61-00-710-109-A
B. Do the test as given in the Para. 3.A.
5. Close-up
Subtask 21-61-00-860-079-A
A. Put the aircraft back to its initial configuration.
[Rev.8 from Aug 2018] 2026.04.04 04:24:54 UTC