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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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Quick Links

04/15/21

Message Overview:

Message Name:

BROKEN SHAFT DETECTION
(Service Message)

Message Code:

B3-303745

Associated CAS:

None

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

Message Description:

Right engine broken shaft detector tripped.

[MCID 1815]
The broken shaft detection system has caused an engine shutdown.

Possible Causes:

  • Broken LP (N1) Shaft
  • Broken Shaft Detector
  • Full Authority Digital Engine Control Unit (FADEC) Electronic Control Unit A (ECU) (A40)
  • 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:

  • Honeywell SIL D201501000039

Quick Links:

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 1815 fault present, troubleshoot using the following steps for aircraft and engine fault isolation with reference to the Light Engine Maintenance Manual Subtask 72-00-00-810-377-A01.
    CAUTION: Do not swap or replace a single FADEC/ECU on an engine that has experienced MCID 1815. Refer to Honeywell SIL D201501000039.

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