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

07/18/19

Message Overview:

Fault Message:

FMQGC DOUBLE ARINC INTERFACE FAULT

Fault Code:

2844679PK

Associated CAS:

None

Reporting LRU: Fuel Management and Quantity Gauging Computer (FMQGC)
System Description: 28-41-00
Schematic Diagram: 28-41-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 31-42-05 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

Fuel Management and Quantity Gauging Computer (FMQGC) DOUBLE ARINC INTERFACE FAULT message shows in CAIMS when one of the following condition occur:

  • Dual ARINC inputs failure from Data Acquisition Unit (DAU) 1 Channel A and Channel B to FMQGC Channel A
  • Dual ARINC inputs failure from Data Acquisition Unit (DAU) 2 CH A and CH B to FMQGC CH B

Possible Causes:

  • Data Acquisition Unit (DAU) 1 (A17)
  • Data Acquisition Unit (DAU) 2 (A18)
  • Junction Box (JB3)
  • Junction Box (JB4)
  • Fuel Management and Quantity Gauging Computer (FMQGC) (A47)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

  1. If FMQGC DOUBLE ARINC INTERFACE FAULT (external fault) is reported in CAIMS and no FMQGS COMPUTER/WRG FAULT (FMQGC Internal Fault) is reported, then the failure is external to the FMQGC. DAU1, DAU2 or the ARINC input wiring is the most probable cause of the failure.
  2. FMQGC internal faults can be checked using CAIMS as follows:

    NOTE: These FMQGC internal faults will trigger the FMQGS COMPUTER/WRG FAULT message in CAIMS.
  3. CAIMS – FMQGC External ARINC Failure Status
  4. FMQGC re-racking procedure

    • The FMQGC pins and mounting tray receptacle have minimal engagement tolerance.Furthermore, the special coaxial pins/sockets used for the fuel probe excitation circuit require additional force to fully engage them. Proper installation and racking of the FMQGC is vital to the operation of the fuel system
    • Install the FMQGC in its mounting tray as follows:

      • Slide the FMQGC straight into the mounting tray until connectors engage
      • Engage the mounting tray turn buckles onto the front of the FMQGC
      • Screw in the turn buckles until the tension increase
      • Placing both hands on the front of the computer, push the FMQGC into the mounting tray
      • Repeat Step c and d several times until the turn buckles are tight and the FMQGC connectors are fully engaged

Quick Links:

Removal of the Junction Box JB3 AMM 24-00-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Junction Box JB3 AMM 24-00-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Junction Box JB3 Circuit-Cards AMM 24-00-02-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Junction Box JB3 Circuit-Cards AMM 24-00-02-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Junction Box JB4 AMM 24-00-05-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Junction Box JB4 AMM 24-00-05-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Junction Box JB4 Circuit-Cards AMM 24-00-06-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Junction Box JB4 Circuit-Cards AMM 24-00-06-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Computer AMM 28-41-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Computer AMM 28-41-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Data Acquisition Units (DAU) AMM 31-42-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Data Acquisition Units (DAU) AMM 31-42-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Using CAIMS - FUEL SYSTEM STATUS Page, determine if the double ARINC input failure is between DAU1 and FMQGC CH A, or DAU2 and the FMQGC CH B.

    1. If the double ARINC input failure is between DAU2 and FMQGC CH B, go to Step 4.
    2. If the double ARINC input failure is between DAU1 and FMQGC CH A, continue with next step.

  2. Swap DAU1 with DAU2.

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

  3. Perform wiring checks between JB3/PCB2, DAU 1 (A17CP1) and FMQGC (A47EP1).
    NOTE: via TP-1,TP-32,TP-63,TP-64 for 93 Pin Testpoint Connector and via TP-1,TP-33,TP-65,TP-66 for 96 Pin Testpoint Connector.

    1. If wiring checks are not good, repair defective wiring as required and do close out.
    2. If fault remains, go to step 6.

  4. Swap DAU2 with DAU1.

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

  5. Perform wiring checks between JB4/PCB2, DAU 2 (A18CP1) and FMQGC (A47EP1).
    NOTE: via TP-1,TP-32,TP-63,TP-64 for 93 Pin Testpoint Connector and via TP-1,TP-33,TP-65,TP-66 for 96 Pin Testpoint Connector.

    1. If wiring checks are not good, repair defective wiring as required and do close out.
    2. If wiring checks are good, continue with next step.

  6. Re-rack the FMQGC.

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

  7. Reset FMQGC power.

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

  8. Replace FMQGC.
  9. Do close out.
Registered and/or unregistered trademarks of Bombardier Inc. or its subsidiaries. © 2015 Bombardier Inc. All rights reserved.