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(WARNING)
RED MESSAGE (CAUTION)
AMBER MESSAGE (ADVISORY)
CYAN MESSAGE (STATUS)
WHITE MESSAGE 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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For AOG assistance contact:

CRC Montreal (YUL)
Quick Links

04/15/21

Message Overview:

Message Name:

POWERPLANT EVENT RECORD

Message Code:

B3-303726

Associated CAS:

None

Reporting LRU: R ENG ECFR
System Description: 76-11-00
Schematic Diagram: None
Wiring Diagram: None

Message Description:

Right engine powerplant event recorded.

[MCID 1813]
The FADEC has recorded a powerplant event.

Possible Causes:

  • Engine Exceeded Redline
  • Pilot Event Marker Activation
  • Auto-Ignition Or Flameout
  • Engine Surge
  • TR Unsafe Detection
  • Commanded High Pressure Shutdown
  • Aborted Ground Start
  • Rejected Takeoff
  • Broken Shaft Event
  • Airborne Engine Start (Windmill or Air Assisted)
  • ECU Records A Degraded Condition
  • Unexpected Change in the ECU Channel in Control
  • A Second ECU Requests a Master Kill

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

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 1813 fault present, troubleshoot using the following steps for aircraft and engine fault isolation with reference to the Light Engine Maintenance Manual TASK 72-00-00-810-368.

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