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Select color for CAS message that you wish to troubleshoot

(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

06/21/23

Message Overview:

L FADEC FAIL
(Caution)

DDG Reference: None
Pilot Action (QRH): ENG 05-9
System Description: 76-11-00
Schematic Diagram: 76-11-00
77-10-00
77-31-00
73-21-00
Wiring Diagram: 73-31-01
77-40-01

Message Description:

The engine control system shows the amber 'L FADEC FAIL' caution CAS message when it determines that any part of the FADEC (both ECUs, all sensors and effectors) has failed.

Possible Causes:

  • Left Engine FADEC common ECU fault
  • Left Engine FADEC common P0 fault
  • Left Engine CGV actuator
  • Left Engine fuel system HMU
  • Left Engine N1 monopole
  • Left Engine surge bleed valve B
  • Left Engine surge bleed valve C
  • Left Engine TT2 sensor/heater
  • Left Engine Anti-ice Valve
  • W5 Harness
  • OSSD Sensor

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

  • AW300-76-0243 - Electronic Control Unit (ECU) Water Ingress (20501 - 20999)

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Removal of the Anti-Ice Pressure Sensor AMM 30-21-03-000-801
Installation of the Anti-Ice Pressure Sensor AMM 30-21-03-400-801
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
Removal of the FADEC Electrical Harness from the Left Engine AMM 71-50-05-000-802
Installation of the FADEC Electrical Harness from the Left Engine AMM 71-50-05-400-802
Removal of the Hydromechanical Unit (HMU) AMM 73-20-01-000-801
Installation of the Hydromechanical Unit (HMU) AMM 73-20-01-400-801
Standard Practices - Wire Repair SPM 20-12-10-02

Troubleshooting Recommendations:

  1. Interrogate the MDC as follows:

    1. On the cursor control panel, ensure the toggle switch is to the right and select Anti-Ice, ECS and Fuel buttons simultaneously. The MDC main menu should now be displayed on Display Unit #3.
    2. Using the joystick, select Current Faults (if the fault is active) or Aircraft History to research stored faults. From Aircraft History you can then select Fault Message History and locate the fault. Going into advanced diagnostics will provide an equation id for the fault identified.
    3. Select the MDC fault or equation from the drop down below to provide additional information to assist in troubleshooting.

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