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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.

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Quick Links

02/16/21

Message Overview:

Message Name:

EGT SENSOR [CIRCUIT 2 XREF FAILURE]

Message Code:

4960153APU

Associated CAS:

APU FAULT
(Advisory)

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

Message Description:

The Auxiliary Power Unit (APU) Full-Authority Digital Engine-Controller (FADEC) detected a failure in the Exhaust-Gas Temperature (EGT) Sensor circuit 2.

Possible Causes:

  • Exhaust Gas Temperature (EGT) Sensor 2 (TC1-2)
  • Auxiliary Power Unit (APU) Full Authority Digital Engine-Controller (FADEC) (A108)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Loss of one EGT sensor will not affect APU operation; however an advisory (Cyan) APU FAULT will be displayed on the EICAS primary page, on ground or in flight. Loss of both EGT will cause an APU SHUTDOWN on ground and an APU FAULT message in flight. EGT sensor can be replaced separately and does not require any adjustments or calibration. It is an 'on condition' component requiring no service.You can access the CAIMS to view the Fault Messages.

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 Exhaust Gas Temperature (EGT) Sensor AMM 49-61-05-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Exhaust Gas Temperature (EGT) Sensor AMM 49-61-05-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Gas Turbine Auxiliary CMM 49-24-35 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

  1. Perform continuity check at the sensor receptacle as per CMM (continuity more than 20 ohms).

    1. If there is no continuity, go to step 6.
    2. If there is continuity, continue with next step.

  2. Examine the engine branched wiring-harness for bare wiring, kinks, worn areas and other damage.

    1. If engine branched wiring-harness is damaged, go to step 7.
    2. If engine branched wiring-harness checks are good, continue with next step.

  3. Perform wiring checks between sensors EGT 2 (TC1-2) and APU FADEC on connector (A108BP1) as follow:

    From To Result
    Chromel (+) A108BP1-K7
    Alumel (-) A108BP1-K8

    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.

  4. Perform wiring checks between APU firewall (J802) and the EGT 2 (TC1-2) sensor as follow:

    From To Expected Result Result
    J802-36 Alumel (-) <6 Ohms
    J802-37 Chromel (+) <6 Ohms

    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.

  5. Perform wiring checks between APU firewall (J802) and the APU FADEC connector (A108BP1) as follow:

    From To Expected Result Result
    J802-37 A108BP1-K7 <11 Ohms
    J802-36 A108BP1-K8 <11 Ohms

    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 EGT 2.

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

  7. Replace or repair engine branched wiring-harness.

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

  8. Replace APU FADEC.
  9. Do close out.
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