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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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10/01/19

Message Overview:

Fault Message:

L OIL FIRE DETECT CH B WRG/PROBE MA

Fault Code:

7327425LBR

Associated CAS:

L FADEC FAULT
(Advisory)

Reporting LRU: Left Engine Electronic Controller (EEC)
System Description: 77-20-00
Schematic Diagram: 77-20-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 71-50-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

The Oil Fire Detection Thermocouple (channel B) has detected failed by the Engine Electronic Controller (EEC) 1. Inhibited during Take-Off and Landing.

Possible Causes:

  • Oil Fire Detection Thermocouple
  • Left Engine Electronic Controller (EEC)

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 ]
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 Bypass-Duct Access Panels
(451AL/461AL, 451BL/461BL, 451CL/461CL,
451DL/461DL, 451EL/461EL, 452FR/462FR,
452GR/462GR, 452HR/462HR, 452JR/462JR,
452KR/462KR)		 AMM 72-71-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Bypass-Duct Access Panels
(451AL/461AL, 451BL/461BL, 451CL/461CL,
451DL/461DL, 451EL/461EL, 452FR/462FR,
452GR/462GR, 452HR/462HR, 452JR/462JR,
452KR/462KR)		 AMM 72-71-01-400-801 [ 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 ]
Removal of the Combustion Section Fairings EMM 73-03-02-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Combustion Section Fairings EMM 73-03-02-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Engine Electronic Controller (EEC) EMM 73-21-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Engine Electronic Controller (EEC) EMM 73-21-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Oil Fire Detection Thermocouple EMM 77-22-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Oil Fire Detection Thermocouple EMM 77-22-01-400-801 [ 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. 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
    ENGINE L T/R CTL VALVE BATT
    ENGINE L T/R LOWER LOCK BATT
    ENGINE L T/R UPPER LOCK BATT

  2. Perform a deactivation of the thrust reverser.
  3. Open the cowls.
  4. Remove the applicable bypass-duct access panel and the applicable combustion section fairing.
  5. Check if the maintenance alert message is stored is stored.

    1. If the maintenance alert message is stored, fault could be intermittent.
    2. If the maintenance alert message is not stored, continue with next step.

  6. Examine the interface wiring for damage between the EEC connector (P1047), the bypass duct connectors (J1032) and (P1032) and the terminal blocks (TB2210), (TB2225) and the ground connector (GC2201) for Channel B.
    NOTE: Look specially for signs of damage adjacent to clip locations.

    1. If there is damage, repair or replace defective wiring as required and go to step 9.
    2. If there is no damage, continue with next step.

  7. Clean the terminal blocks TB2210 and TB2225, and the ground connector (GC2201) and the Alumel and Chromel terminal lugs. Check if the fault message is still active.

    1. If the fault message is not active, go to step 9.
    2. If the fault message is active, continue with next step.

  8. Replace oil-fire detection thermocouple.
  9. Close the cowls.
  10. Perform a activation of the thrust reverser.
  11. Do close out.

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