W DOC AIRBUS | TSM A320F

Failure of the Angle of Attack Sensor (PHC 1)


TASK 30-31-00-810-808-A
Failure of the Angle of Attack Sensor (PHC 1)


1. Possible Causes
  • SENSOR-ANGLE OF ATTACK, 1 [3FP1]
  • PHC-1 [6DA1]
  • wiring from the PHC 1 (6DA1) to the angle of attack sensor 1 (3FP1)
  • wiring
  • ADIRU-1 [1FP1]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 30-31-00-710-001
Operational Test of the Probe Ice Protection
AMM 30-31-00-710-007
Functional Test of the Heating of the Angle of Attack Sensor
AMM 30-31-00-710-802
Functional Test of the Heating of the Angle of Attack Sensor
ASM 303101
AMM 30-31-34-000-002
Removal of the Probe Heat Computer (PHC)
AMM 30-31-34-400-002
Installation of the Probe Heat Computer (PHC)
AMM 34-11-19-000-001
Removal of the Angle of Attack Sensor
AMM 34-11-19-400-001
Installation of the Angle of Attack Sensor
AMM 34-12-34-000-001
Removal of the ADIRU
AMM 34-12-34-400-001
Installation of the ADIRU
ASM 341302
3. Fault Confirmation
Subtask 30-31-00-710-064-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the functional test of the heating of the angle of attack sensor AMM 30-31-00-710-007.
Subtask 30-31-00-710-064-B ** ON A/C NOT FOR ALL
A. Test
   (1) Do the functional test of the heating of the angle of attack sensor AMM 30-31-00-710-802.
4. Fault Isolation
Subtask 30-31-00-810-057-A
A. If the measured in-rush current is less than 1.3A during approximately 30 seconds or more than 9A during approximately 10 seconds:
   (1) Replace the SENSOR-ANGLE OF ATTACK, 1 [3FP1] AMM 34-11-19-000-001 and AMM 34-11-19-400-001.
Subtask 30-31-00-810-125-A
B. If none of the results recorded is less than 1.3A or more than 9A:
   (1) Replace the PHC-1 [6DA1] AMM 30-31-34-000-002 and AMM 30-31-34-400-002.
   (2) If the fault continues:
  • do a check and repair the wiring from the PHC 1 (6DA1) to the angle of attack sensor 1 (3FP1) , pin A/F to pin A/<J ASM 303101.
   (3) If the fault continues:
     (a) Disconnect connector A from PHC 1 and remove ADIRU 1 AMM 34-12-34-000-001.
     (b) Do a check of the probe signal wiring ASM 341302 between PHC 1 pin A/Z and ADIRU 1 pin AA/3J.
       1 If there is no continuity:
       2 If there is continuity:
Subtask 30-31-00-710-065-A
C. Do the operational test of the probe ice protection AMM 30-31-00-710-001.
[Rev.8 from Aug 2018] 2026.04.04 04:29:34 UTC