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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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For AOG assistance contact:

CRC Montreal (YUL)
Quick Links

01/28/21

Message Overview:

R STARTER FAIL ON
(Caution)

DDG Reference: None
Pilot Action (QRH): NNC-15-6
System Description: 80-10-00
Schematic Diagram: 80-11-00
Wiring Diagram: 80-11-01
80-11-03

Message Description:

The amber 'R STARTER FAIL ON' caution CAS message indicates the respective engine starter has failed on.

  • The ECU has commanded the starter control valve solenoid to close and has not received close logic from the starter control valve position switch.

Possible Causes:

  • Full Authority Digital Engine Control (FADEC) Electronic Control Unit A (ECU) (A40)
  • Full Authority Digital Engine Control (FADEC) Electronic Control Unit B (ECU) (A42)
  • Starter Control Valve Solenoid
  • Starter Control Valve Position Switch
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Engine Starting System - Component Location AMM 80-11-00-992-801
Removal of the Air Turbine Starter AMM 80-11-01-000-801
Installation of the Air Turbine Starter AMM 80-11-01-400-801
Starter-Control-Valve Manual-Override Procedure AMM 80-11-05-860-801
Removal of the Starter Control Valve AMM 80-11-05-000-801
Installation of the Starter Control Valve AMM 80-11-05-400-801
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.

45_advance_diagnostics20_air_turbine_assembly

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