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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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09/28/19

Message Overview:

Fault Message:

R SAV CH A WRG/SAV [SOL] RNG MA

Fault Code:

7327316RBR

Associated CAS:

None

Reporting LRU: Right 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:

An electrical fault in the Starter Air Valve (SAV) Solenoid has been detected by the Engine Electronic Controller (EEC) 2 CH A. Inhibited during Take-Off and Landing.

Possible Causes:

  • Right Starter Air Valve (SAV)
  • Right Engine Electronic Controller (EEC)
  • Secondary Power Distribution Assembly (SPDA) 3 (A15)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

Forum Articles/Infoservice/Newsletter: None

NOTE: Both Ch A and CH B SAV solenoid circuits faults must be detected to set the R ENG SAV FAIL (Amber) CAS message.

Quick Links:

Removal of the Secondary-Power Distribution
Assemblies		 AMM 24-62-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Secondary-Power Distribution
Assemblies		 AMM 24-62-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
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 ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Open the engine Cowls.
  2. Measure for 28 VDC at the RH SAV solenoid channel A (P1065).

    1. If there is 28 VDC, go to step 4 (when the SAV is commanded open).
    2. If there is no 28 VDC, continue with next step.

  3. Perform wiring checks between the SPDA 3 (A15P1) and the EEC 1 (P1045).

    1. If wiring checks are not good, repair defective wiring as required and go to step 8.
    2. If wiring checks are good, continue with next step.

  4. Perform wiring checks between the EEC 2 (P1043) and the RH SAV (P1065).

    1. If wiring checks are not good, repair defective wiring as required and go to step 8.
    2. If wiring checks are good, continue with next step.

  5. Swap the SPDA 3 with the SPDA 2. Is the fault still present?

    1. If NO, replace SPDA 3 and go to step 8.
    2. If YES, continue with next step.
      NOTE: You may swap if there is no 28 VDC between the SPDA 3 and the EEC 2.

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

    1. If NO, replace Right SAV and go to step 8.
    2. If YES, continue with next step.

  7. Replace the EEC 2.
  8. Close the cowls.
  9. Do close out.

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