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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

09/27/19

Message Overview:

Fault Message:

L SAV CH A WRG/SAV [SOL] RNG

Fault Code:

7326116LBR

Associated CAS:

L ENG SAV FAIL
(Caution)

Reporting LRU: EEC 1
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 EEC 1 CH A. Inhibited during Take Off and Landing.

Possible Causes:

  • Starter Air Valve (SAV)
  • Engine Electronic Controller (EEC)1
  • Secondary Power Distribution Assemblies (SPDA) 2
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

  • Check the wiring between the Starter Air Valve (SAV) and the EEC prior to replacing an EEC.

Quick Links:

Removal of the Engine Electronic Controller (EEC) EMM 73-21-01-000-801
Installation of the Engine Electronic Controller (EEC) EMM 73-21-01-400-801
Removal of the Starter Air Valve EMM 80-11-03-000-801
Installation of the Starter Air Valve EMM 80-11-03-400-801
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 ]
Wire Repair SPM 20-12-10 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

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

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

  3. Perform wiring checks between the SPDA 2 (A14P1) and the EEC 1 (P1045).

    1. If system checks are good, do close out.
    2. If fault remains, continue with next step.

  4. Perform wiring checks between the EEC 1 (P1043) and the LH SAV (P1065).

    1. If system checks are good, do close out.
    2. If fault remains, continue with next step.

  5. Swap the SPDA 2 with the SPDA 3.

    1. If system checks are good, do close out.
    2. If fault remains, continue with next step.
      NOTE: You swap if there is no 28 VDC between the SPDA 2 and the EEC 1.

  6. Swap SAV between engines.

    1. If system checks are good, do close out.
    2. If fault remains, continue with next step.

  7. Replace the EEC 1.
  8. Do close out.
    starter_air_valve_ch_a

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