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(ADVISORY)
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(STATUS)
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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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For AOG assistance contact:

CRC Montreal (YUL)
Quick Links

07/21/25

Message Overview:

Message Name:

R ITT CH A WRG/PROBE RNG MA

Message Code:

7327228RBR

Associated CAS:

EEC software C6 & C7

None

 EEC software C8 & X

R FADEC FAULT
(ADVISORY)

Reporting LRU: Engine Electronic Controller (EEC) 2
System Description: 77-20-00 - Temperature
Schematic Diagram: [ Global Express ]  [ G5000 ]  [ Global XRS ] SMM 77-20-00-101 - Engine Temperature Indicating System - Electrical Schematic
Wiring Diagram: [ Global Express ]  [ G5000 ]  [ Global XRS ] WM 71-50-00-01 - Engine Electrical Harness
[ Global Express ]  [ G5000 ]  [ Global XRS ] WM 77-20-00-01 - Engine Temperature Indicating System

Message Description:

There is an open or short circuit in the interface wiring. The Inter-Turbine Temperature (ITT) circuits are continuously monitored by the Full-Authority Digital Engine-Controller (FADEC).

Possible Causes:

  • Inter-Turbine Temperature (ITT) Thermocouples
  • Right Engine Electronic Controller (EEC)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Full Throttle Blog/Forum Articles/Infoservice/Newsletter: None

Flight Operation Notifications Manual (FONM): None

NOTES:

  • If lost of ITT indication on the EICAS display due to the CHA and/or CHB failure; Dashes will appear instead of the indication.

Quick Links:

Connect Electrical Power to the Aircraft [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-861-801
Remove the Electrical Power from the Aircraft [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-861-802
Access to Active Faults [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-802
Access to Stored Faults [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM45-45-00-970-803
Standard Aircraft Configuration for Maintenance [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM12-00-00-867-801
Aircraft Walkaround (for Maintenance) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM12-00-00-867-802
Connect Electrical Power to the Aircraft [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-861-801
Remove the Electrical Power from the Aircraft [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-861-802
Opening of Non-Thermal Circuit Breakers [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-863-801
Closing of Non-Thermal Circuit Breakers [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-863-802
Electrostatic Discharge Safety Precautions [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM24-00-00-910-802
Engine Safety Precautions [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM71-00-00-910-801
Opening of the Cowls (432AB/442AB, 432AT/442AT) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM71-10-00-010-801
Closing of the Cowls (432AB/442AB, 432AT/442AT) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM71-10-00-410-801
Removal of the Bypass-Duct Access Panels (451AL/461AL, 451BL/461BL, 451CL/461CL, 451DL/461DL, 451EL/461EL, 452FR/462FR, 452GR/462GR, 452HR/462HR, 452JR/462JR, 452KR/462KR) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM72-71-01-000-801
Installation of the Bypass-Duct Access Panels (451AL/461AL, 451BL/461BL, 451CL/461CL, 451DL/461DL, 451EL/461EL, 452FR/462FR, 452GR/462GR, 452HR/462HR, 452JR/462JR, 452KR/462KR) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM72-71-01-400-801
Deactivation of the Thrust Reverser (for Maintenance) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM78-30-00-040-801
Reactivation of the Thrust Reverser (for Maintenance) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM78-30-00-440-801
Standard Aircraft Configuration for Maintenance [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM12-00-00-867-801
Aircraft Walkaround (for Maintenance) [ G5000 ]  [ Global Express ]  [ Global XRS ] AMM12-00-00-867-802

Troubleshooting Recommendations:

  1. Perform a visual inspection of the ITT Thermocouple.
    NOTE: Look specially for signs of damage adjacent to clip locations and corrosion around the ceramic insulator. Refer to image below that shows clean and contaminated TGT Thermocouple.

    1. If damage or defect are found, rectify or repair as required and do close out.
    2. If damage or defect are not found, continue with next step.

  2. Interchange EECs.

    1. If system checks are good, replace the defective EEC and do close out.
    2. If fault remains continue with the next step.

  3. Disconnect the EEC connector (P1044) and the bypass duct connector (P1030 and J1030). Disconnect the interface wiring at the terminal blocks TB2112 and TB2113. Perform a visual inspection of the wiring and connectors for damage between the connectors and the terminal blocks.
    NOTE: Look for signs of chafing adjacent to clip locations, condition of connector pins and wiring kink or strain.

    1. If defects are found, rectify or repair as required and do close out.
    2. If defects are not found, continue with next step.

  4. Perform a continuity check between the terminal blocks Chromel and Alumel terminal lugs (TB2112 and TB2113) and the connector P1030 as follows:

    From To Result
    TB2112 P1030-16
    TB2113 P1030-17

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  5. Perform a continuity check between the connectors J1030 and P1044 as follows:

    From To Result
    J1030-16 P1044-50
    J1030-17 P1044-29

    1. If there is no continuity, repair defective wiring as required and do close out.
    2. If there is continuity, continue with next step.

  6. Disconnect Thermocouple (Ladder) Harness from the Thermocouples.
    thermocouple_harness
  7. Do wiring check of Thermocouple (Ladder) Harness for continuity.

    1. If Harness has continuity between all connection points replace the defective TGT Thermocouple.
    2. If Thermocouple Harness does not have continuity between connection points replace Thermocouple Harness. 

  8. Make sure that the primary indication of ITT shows on the EICAS display.
  9. Do close out.
    itt_low
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