04/14/21
Message Overview:
Message Name:
FADEC PMA POWER A
Message Code:
B3-303444
Associated CAS:
| Reporting LRU: | L ENG ECU A |
| System Description: | 76-11-00 |
| Schematic Diagram: | None |
| Wiring Diagram: | None |
Message Description:
Left engine FADEC PMA power fault A.
[MCID 0928]
FADEC PMA Power A.
A fault in the ECU A or the PMA was sensed.
Possible Causes:
- Full Authority Digital Engine Control Unit (FADEC) Electronic Control Unit A (ECU) (A41)
- Wiring Harness (W6)
- Wiring Harness (W4)
- Wiring Harnesses from the AIRCRAFT INTERFACE to the Engine RUN Switch
- Engine RUN Switch
- Permanent-Magnet-Alternator (PMA) Power A
- Associated Wiring
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
Quick Links:
| General Visual Inspection of the Engine Wiring Harness | AMM 71-50-00-210-802 |
| Removal of the FADEC Electrical Harness from the Left Engine | AMM 71-50-05-000-802 |
| Installation of the FADEC Electrical Harness on the Left Engine | AMM 71-50-05-400-802 |
| Removal of the Engine Electronic Control Unit (ECU) | AMM 76-10-05-000-801 |
| Installation of the Engine Electronic Control Unit (ECU) | AMM 76-10-05-400-801 |
| Wiring - Maintenance Practices - ALL | SPM 20-12-00-02 |
| Wire Repair - Maintenance Practices - ALL | SPM 20-12-10-02 |
| Electrical Connectors - Maintenance Practice - ALL | SPM 20-20-00-02 |

