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

08/28/19

Message Overview:

Fault Message:

R OIL FIRE CH B WRG/PROBE RNG

Fault Code:

7325316RBR

Associated CAS:

R FADEC FAIL
(Caution)

Reporting LRU: EEC 2
System Description: 77-20-00
Schematic Diagram: None
Wiring Diagram: 71-50-01 [ Global Express ]  [ Global XRS ]  [ G5000 ]

Fault Description:

The oil fire detection thermocouple (channel B) has detected failed by the EEC 1. Inhibited during Take-off and Landing.

Possible Causes:

  • Oil Fire Detection Thermocouple
  • Engine Electronic Controller (EEC)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Check the wiring between the oil fire detection thermocouple 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 Oil Fire Detection Thermocouple EMM 77-22-01-000-801
Installation of the Oil Fire Detection Thermocouple EMM 77-22-01-400-801
Removal of the Turbine Overheat-Detection Thermocouple EMM 77-23-01-000-801
Installation of the Turbine Overheat-Detection Thermocouple EMM 77-23-01-400-801
Wire Repair SPM 20-12-10 [ Global Express ]  [ Global XRS ]  [ G5000 ]

Troubleshooting Recommendations:

CAUTION: DO NOT PERFORM 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 R FADEC CH A BATT
    ENGINE R FADEC CH B BATT
    ENGINE R ENG IGN 1 BATT
    ENGINE R ENG IGN 2 BATT
    ENGINE R ENG FUEL HPSOV BATT
    ENGINE R ENG START A BATT
    ENGINE R ENG START B BATT
    ENGINE R T/R CTL VALVE BATT
    ENGINE R T/R LOWER LOCK BATT
    ENGINE R T/R UPPER LOCK BATT

  2. Do a deactivation of the thrust reverser.
  3. Open the cowls.
  4. Remove the applicable bypass−duct access panel.
  5. Remove the applicable combustion section fairing.
  6. If the maintenance alert message is stored, the fault could be intermittent.
  7. Examine the interface wiring for damage between the connectors and the terminal blocks that follow:

      For Channel B

    • The EEC connector P1047
    • The bypass duct connectors J1032 and P1032
    • The terminal blocks TB2210 and TB2225, and the ground connector GC2201

    NOTE: Look for signs of damage adjacent to clip locations.

  8. Clean the terminal blocks TB2210 and TB2225, the ground connector GC2201 and the Alumel and Chromel terminal lugs
  9. Repair or replace defective wiring as necessary.
  10. If the fault message is still active, replace the oil-fire detection thermocouple .
  11. Do close out.

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