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

09/17/19

Message Overview:

Fault Message:

SHORT - INLET PRESS SENSOR/EXC WRG

Fault Code:

4960181APU

Associated CAS:

None

Reporting LRU: Full-Authority Digital Engine-Controller (FADEC)
System Description: 49-60-00
Schematic Diagram: 49-61-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 49-12-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]
49-61-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

The Inlet Pressure Sensor excitation load resistance read by the Full-Authority Digital Engine-Controller (FADEC) is out of range low. This shows a possible short in the Inlet Pressure Sensor excitation or the engine branched wiring-harness.

Possible Causes:

  • Auxiliary Power Unit (APU) Full-Authority Digital Engine-Controller (FADEC) (A108)
  • Inlet Pressure Sensor (MT1)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

APU Safety Precautions AMM 49-00-00-910-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Engine Branched Wiring-Harness AMM 49-12-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Engine Branched Wiring-Harness AMM 49-12-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Full-Authority Digital Engine-Controller (FADEC) AMM 49-61-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Full-Authority Digital Engine-Controller (FADEC) AMM 49-61-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Inlet Pressure Sensor AMM 49-61-13-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Inlet Pressure Sensor AMM 49-61-13-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Examine the engine branched wiring-harness for bare wiring, kinks, worn areas and other damage (WM 49-12).

    1. If there is bare wiring, kinks, worn areas or other damage, go to step 6.
    2. If NO, continue with next step.

  2. Examine the inlet pressure sensor (MT1) receptacle for contamination and damage.

    1. If contaminated or damaged, go to step 7.
    2. If NO, continue with next step.

  3. Perform a continuity check within the inlet pressure sensor (MT1) receptacle as follows:

    From To Expected Result Result
    MT1P1-C MT1P1-D >20 ohms

    1. If checks are not good, go to step 7.
    2. If checks are good, continue with next step.

  4. Perform a wiring check between P802 (APU) and MT1P1 (inlet pressure sensor).

    1. If wiring checks are not good, go to step 6.
    2. If wiring checks are good, continue with next step.

  5. Perform a wiring check between J802 (AC wiring harness) and A108AP1 (FADEC).

    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. Replace Engine branched wiring-harness.

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

  7. Replace the inlet pressure sensor (MT1).

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

  8. Replace FADEC (A108).
  9. Do close out.
Registered and/or unregistered trademarks of Bombardier Inc. or its subsidiaries. © 2015 Bombardier Inc. All rights reserved.