DOC AIRBUS | TSM A320FLoss of the R Static Probe Output-Discrete from the PHC 2
TASK 30-31-00-810-849-A
Loss of the R Static Probe Output-Discrete from the PHC 2
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 30-31-00-710-146-A 4. Fault Isolation
Subtask 30-31-00-810-098-A
[Rev.8 from Aug 2018]
2026.04.04 04:29:38 UTC
Loss of the R Static Probe Output-Discrete from the PHC 2
1. Possible Causes
- PHC-2 [6DA2]
wiring from the PHC 2 (6DA2) to the ADIRU 2 (1FP2)
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 30-31-00-710-001 | Operational Test of the Probe Ice Protection |
| ASM 303102 | |
| 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 34-13-00-740-002 | INTERFACE TEST of the ADR |
| ASM 341302 |
Subtask 30-31-00-710-146-A 4. Fault Isolation
Subtask 30-31-00-810-098-A
A. If the test gives the maintenance message CHECK ADIRU2 R STATIC PHC 2 INTERFACE:
Subtask 30-31-00-710-147-A - do a check for ground at pin A/Y of the PHC 2 (6DA2) ASM 303102.
- replace the PHC-2 [6DA2] , AMM 30-31-34-000-002 and AMM 30-31-34-400-002.
- do a check and repair the
wiring from the PHC 2 (6DA2) to the ADIRU 2 (1FP2) pin A/Y to pin AA/4H ASM 341302.
- do the INTERFACE TEST of the ADR (system 2) AMM 34-13-00-740-002
- do the necessary corrective actions: (TSM chapter 34).
B. Do the operational test given in Para. 3.