07/26/19
Message Overview:
| DDG Reference: | None |
| Pilot Action (QRH): | ADVISORY 12-9 |
| System Description: | 31-40-00 |
| Schematic Diagram: | 31-41-00 [ Global Express ] [ G5000 ] [ Global XRS ] |
| Wiring Diagram: | 31-41-02 [ Global Express ] [ G5000 ] [ Global XRS ] |
Fault Description:
The internal temperature of an IAC 1 is higher than the safe maximum limit of approximately 72°C.
Possible Causes:
- The ventilation inlet and/or cooling fan of Integrated Avionics Computer (IAC) 1 has a blockage
- Integrated Avionics Computer (IAC) 1 Battery
- Integrated Avionics Computer (IAC) 1 Configuration Module
- Integrated Avionics Computer (IAC) 1
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
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:
- On the CAIMS PMAT, get access to system diagnostics (AMM TASK 45-45-00-970-804) and do the IAC EDS/Core Test.
- After each test is completed, look for the TEST RESULTS page and record the fault type and code(s) for each IMT fault.
- Do the IMT fault code look-up procedure (AMM TASK 45-45-00-970-826) to find the applicable troubleshooting procedures.
- Carry out troubleshooting procedures.
- Do close out.