background
x
loader
Troubleshooting
arrow By ATA By Message Color By Observed Faults by MDCBy 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

02/03/21

Message Overview:

Message Name:

NO OUTPUT

Message Code:

B3-006731

Associated CAS:

None

Reporting LRU: FGC 2
System Description: 22-11-00
Schematic Diagram: 22-11-00
Wiring Diagram: 31-45-01

Message Description:

The right Input/Output Concentrator #2 (IOC 2) data bus inputs from the flight guidance computer #2 (FGC 2) are inactive.

Possible Causes:

  • Right Flight Guidance Computer (FGC) 2 (A4-FGC)
  • Right Input/Output Concentrator Unit (IOC) 2 (A4-IOC)
  • Right Integrated-Avionics Processor System (IAPS) Power Supply (PWR 2) (A4-PWR)
  • Integrated-Avionics Processor System (IAPS) Card Cage (ICC) (A4)

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Removal of Flight Guidance Computer (FGC) AMM 22-11-01-000-801
Installation of Flight Guidance Computer (FGC) AMM 22-11-01-400-801
Removal of Integrated Avionics Processor System (IAPS) Card Cage (ICC) AMM 31-45-01-000-801
Installation of Integrated Avionics Processor System (IAPS) Card Cage (ICC) AMM 31-45-01-400-801
Removal of Input/Output Concentrator Unit (IOC) AMM 31-45-05-000-801
Installation of Input/Output Concentrator Unit (IOC) AMM 31-45-05-400-801
Removal of the Integrated Avionics Processor System (IAPS) Power Supply (PWR) AMM 31-45-09-000-801
Installation of the Integrated Avionics Processor System (IAPS) Power Supply (PWR) AMM 31-45-09-400-801

Troubleshooting Recommendations:

  1. Reset R IAPS Circuit Breaker CB2-B6. Is the fault message still present?

    1. If YES, continue with next step.
    2. If NO, do close out.
      NOTE: Before you open the IAPS circuit breakers, make sure that all Engine FADEC circuit breakers are open. If the Engine FADEC circuit breakers remain closed, Engine Igniters will activate. This can cause injury to persons and damage to equipment.

  2. Swap Right FGC with Left FGC. Is the fault message still present?

    1. If YES, continue with next step.
    2. If NO, replace defective FGC.

  3. Swap Right IOC with Left IOC. Is the fault message still present?

    1. If YES, continue with next step.
    2. If NO, replace defective IOC.

  4. Swap IAPS PWR 2 with IAPS PWR 1. Is the fault message still present?

    1. If YES, continue with next step.
    2. If NO, replace defective IAPS PWR.

  5. Replace IAPS card cage (A4).
  6. Do close out.

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