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Require immediate crew attention. These messages are accompanied by flashing master warning, triple chime attenson with or without voice message or dedicated tone. Require immediate crew awareness and future crew action may be required in the form of alternate system selection or performance limitation. These message are accompanied by flashing master caution and a single chime. Indicate safe or normal system operation which require crew awareness, over and above the dark cockpit philosophy. Indicate minor failures or reduction in systems capability, which require no crew action.

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04/14/21

Message Overview:

Message Name:

ENGINE PMA 1B

Message Code:

B3-303664

Associated CAS:

R ENGINE MINOR FAULT
(Advisory)

Reporting LRU: R ENG PMA
System Description: 76-20-00
Schematic Diagram: None
Wiring Diagram: None

Message Description:

Right engine PMA fault 1B

[MCID 0904]
Engine PMA 1B.
Detection of a fault in the Permanent Magnet Alternator harness between the PMA and the ECU B. The ECU B cannot support full system operation.

Possible Causes:

  • Permanent Magnet Alternator (PMA)
  • Wiring Harness (W6)
  • Wiring Harness (W4)
  • Full Authority Digital Engine Control Unit (FADEC) Electronic Control Unit B (ECU) (A42)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Component Location AMM 28-41-00-992-801
General Visual Inspection of the Engine Wiring Harness AMM 71-50-00-210-802
Removal of the FADEC Electrical Harness from the Right Engine AMM 71-50-05-000-803
Installation of the FADEC Electrical Harness on the Right Engine AMM 71-50-05-400-803
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

Troubleshooting Recommendations:

  1. MCID 0904 fault present, troubleshoot using the following steps for aircraft and engine fault isolation with reference to the Light Engine Maintenance Manual Subtask 72-00-00-810-132-A01.
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