background
x
loader
Troubleshooting
arrow By ATA By Message Color By Observed Faults By CAIMS By Tips

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.

This page includes :

For AOG assistance contact:

CRC Montreal (YUL)
Quick Links

09/26/19

Message Overview:

Fault Message:

L STARTER MOTOR

Fault Code:

7326220LBR

Associated CAS:

L FADEC FAIL
(Caution)

Reporting LRU: Left Engine Electronic Controller (EEC)
System Description: 80-11-00
Schematic Diagram: 80-11-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 71-50-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

The fault message is set during the engine start procedure when:

  • The Full-Authority Digital Engine-Controller (FADEC) senses no accelerating torque input
  • N2 does not get to starter cut-out speed in the specified time limit

This is when all other engine start system limits are in the specified limits.

Possible Causes:

  • Left Starter Air Valve (SAV)
  • Left Engine Electronic Controller (EEC)
  • Left Air Turbine Starter
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Opening of the Cowls AMM 71-10-00-010-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Closing of the Cowls AMM 71-10-00-410-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Eng Electronic Controller (EEC) Mod 73-101559 EMM 73-21-01-000-801-B00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Eng Electronic Controller (EEC) Mod 73-101559 EMM 73-21-01-400-801-B001 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Starter Air Valve EMM 80-11-03-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Starter Air Valve EMM 80-11-03-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Air Turbine Starter EMM 80-11-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Air Turbine Starter EMM 80-11-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Open the engine cowls
  2. Perform wiring checks between the EEC 1 (P1043 and P1046) and the LH SAV (P1065 and P1066)

    1. If wiring checks are not good, repair defective wiring as required and do close out.
    2. If wiring checks are good, continue with next step.

  3. Swap the Left SAV with Right SAV engines. Is the fault still present?

    1. If NO, replace Left SAV and do close out.
    2. If YES, continue with next step.

  4. Swap the EEC 1 with EEC 2. Is the fault still present?

    1. If NO, replace EEC 1 and do close out.
    2. If YES, continue with next step.

  5. Replace the LH Air Turbine Starter.
  6. Close the engine cowl.
  7. Do close out.

Registered and/or unregistered trademarks of Bombardier Inc. or its subsidiaries. © 2015 Bombardier Inc. All rights reserved.