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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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10/07/19

Message Overview:

Fault Message:

L ENG [N1 SPEED PROBE]/WIRING

Fault Code:

7735316BRV

Associated CAS:

None

Reporting LRU: Engine Vibration-Monitoring Unit (EVMU)
System Description: 77-30-00
Schematic Diagram: 77-31-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 71-50-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]
77-31-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

The fault message is set when there is a problem with the N1 speed input to the Engine Vibration-Monitoring Unit (EVMU).

Possible Causes:

  • N1 Speed Probe
  • Engine Vibration-Monitoring Unit (EVMU) (A42)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Engine Safety Precautions AMM 71-00-00-910-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Start the Engine AMM 71-00-00-866-806 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Engine Shutdown (Usual) AMM 71-00-00-866-809 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Power Plant AMM 71-00-00-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Power Plant AMM 71-00-00-400-801 [ 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 Engine Vibration-Monitoring Unit (EVMU) AMM 77-31-04-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Engine Vibration-Monitoring Unit (EVMU) AMM 77-31-04-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Thrust Reverser Safety Precautions AMM 78-30-00-910-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Deactivation of the Thrust Reverser (for Maintenance) AMM 78-30-00-040-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Activation of the Thrust Reverser (for Maintenance) AMM 78-30-00-440-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

CAUTION: DO NOT DO ELECTRICAL CHECKS INTO THE ENGINE ELECTRONIC CONTROLLER (EEC). IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE EEC CAN OCCUR.

  1. Remove the electrical power from the aircraft.
  2. In the flight compartment, on the EMS CDU, open the circuit breakers that follow:

    System Name Circuit Breaker Name Bus Name
    ENGINE L FADEC CH A BATT
    ENGINE L FADEC CH B BATT
    ENGINE L ENG IGN 1 BATT
    ENGINE L ENG IGN 2 BATT
    ENGINE L ENG FUEL HPSOV BATT
    ENGINE L ENG START A BATT
    ENGINE L ENG START B BATT
    THRUST REV L T/R CTL VALVE BATT
    THRUST REV L T/R LOWER LOCK BATT
    THRUST REV L T/R UPPER LOCK BATT

  3. Perform a deactivation of the thrust reverser and open the cowls.
  4. Perform a visual inspection of the interface wiring, terminals and connectors for damage between EVMU (A42BP1) and N1 speed probes (P711).
    NOTE: Look specially for signs of damage adjacent to clip locations, condition of connector pins and wiring that is kinked or strained.

    1. If any damage found, repair or replace as required and go to step 16.
    2. If no damage and the fault message was stored in the Fault Confirmation above, then the fault could be intermittent and continue with next step.

  5. Monitor the system to see if the fault message occurs again.

    1. If the fault message is not active, go to step 16.
    2. If the fault message is active, continue with next step.

  6. Perform wiring checks between N1 Speed Probe (P711) and Fixed Cowl Interface (1PB2).

    1. If wiring checks are not good, repair defective wiring as required and go to step 16.
    2. If wiring checks are good, continue with next step.

  7. Perform wiring checks between F ixed Cowl Interface (1JB2) and A ft Pressure Bulkhead STN 861 LHS (P607).

    1. If wiring checks are not good, repair defective wiring as required and go to step 16.
    2. If wiring checks are good, continue with next step.

  8. Perform wiring checks between Fixed Cowl Interface (2JB2) and A ft Pressure Bulkhead STN 861 RHS (P608).

    1. If wiring checks are not good, repair defective wiring as required and go to step 16.
    2. If wiring checks are good, continue with next step.

  9. Perform wiring checks between Aft Pressure Bulkhead STN 861 LHS (J607) and EVMU (A42BP1).

    1. If wiring checks are not good, repair defective wiring as required and go to step 16.
    2. If wiring checks are good, continue with next step.

  10. Check for fault message L ENG [N1 SPEED PROBE]/WIRING.

    1. If the fault is not active, go to step 16.
    2. If the fault stays active, continue with next step.

  11. Perform a check for the insulation resistance of the interface between the connectors N1 Speed Probe to Fixed Cowl Interface.

    From To Expected Result Result
    P711-1 Ground >20 megaohms
    P711-2 Ground >20 megaohms

    1. If the resistance value is out of limit, repair defective wiring as required and go to step 16.
    2. If the resistance value is within limit, continue with next step.

  12. Perform a check for the insulation resistance of the interface between the connectors Fixed Cowl Interface to Aft Pressure Bulkhead.

    From To Expected Result Result
    P607-r Ground >20 megaohms
    P607-s Ground >20 megaohms

    1. If the resistance value is out of limit, repair defective wiring as required and go to step 16.
    2. If the resistance value is within limit, continue with next step.

  13. Perform a check for the insulation resistance of the interface between the connectors Aft Pressure Bulkhead to EVMU.

    From To Expected Result Result
    A42BP1-A1 Ground >20 megaohms
    A42BP1-B1 Ground >20 megaohms

    1. If the resistance value is out of limit, repair defective wiring as required and go to step 16.
    2. If the resistance value is within limit, continue with next step.

  14. Replace EVMU.

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

  15. Replace the power plant.
  16. Close the cowls and activate the Thrust Reverser.
  17. Do close out.
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