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

08/05/19

Message Overview:

Fault Message:

FWC 1 - INTERNAL IOP FAULT

Fault Code:

3151010FW1

Associated CAS:

IAC 1 OVHT
(Caution)

SG 1 FAIL
(Caution)

AFCS 1 FAIL
(Advisory)

FMS 1 FAIL
(Advisory)

Reporting LRU: Integrated Avionics Computer (IAC) 1
System Description: 31-40-00
Schematic Diagram: 31-41-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 31-41-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

The internal temperature of Integrated Avionics Computer (IAC) 1 is higher than the safe maximum limit of approximately 72°C.

Possible Causes:

  • Integrated Avionics Computer (IAC) 1 (A11)
  • Integrated Avionics Computer (IAC) 1 Ventilation Inlet
  • Integrated Avionics Computer (IAC) 1 Cooling Fan
  • Integrated Avionics Computer (IAC) 1 Battery
  • Integrated Avionics Computer (IAC) 1 Configuration Module (A41)

Troubleshooting Tips:

Advisory Wire/Service Bulletin:

Forum Articles/Infoservice/Newsletter: None

NOTE: In this condition, IAC 1 can possibly transmit incorrect data to other aircraft systems

Quick Links:

Access to Active Faults AMM 45-45-00-970-802 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Access to System Diagnostics AMM 45-45-00-970-804 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Integrated Maintenance Test (IMT) Fault Code Look-Up AMM 45-45-00-970-826 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. On the CAIMS PMAT, get access to system diagnostics and do the IAC EDS/Core Test.
  2. After each test is completed, look for the TEST RESULTS page and record the fault type and code(s) for each IMT fault.
  3. Perform the IMT fault code look-up procedure to find the applicable troubleshooting procedures.
  4. Carry out troubleshooting procedures.
  5. Do close out.

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