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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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09/25/19

Message Overview:

Fault Message:

L ITT SIGNAL CH B RNG

Fault Code:

7325726LBR

Associated CAS:

None

Reporting LRU: Left Engine Electronic Controller (EEC)
System Description: 77 -20-00
Schematic Diagram: 77-20-00 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wiring Diagram: 71-50-01 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Fault Description:

There is a failure of the signals from channel B of the Inter-Turbine Temperature (ITT) Thermocouples. The ITT circuits are continuously monitored by the Full-Authority Digital Engine-Controller (FADEC).

Possible Causes:

  • Inter-Turbine Temperature (ITT) Thermocouple
  • Left Engine Electronic Controller (EEC)
  • Associated Wiring

Troubleshooting Tips:

Advisory Wire/Service Bulletin: None

Forum Articles/Infoservice/Newsletter: None

Quick Links:

Engine Safety Precautions AMM 71-00-00-910-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Opening of the Cowls AMM 71-10-00-010-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Closing of the Cowls AMM 71-10-00-410-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
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)
AMM 72-71-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
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)
AMM 72-71-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Deactivation of the Thrust Reverser (for Maintenance) AMM 78-30-00-040-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Activation of the Thrust Reverser (for Maintenance) AMM 78-30-00-440-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Combustion Section Fairings EMM 73-03-02-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Combustion Section Fairings EMM 73-03-02-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Engine Electronic Controller (EEC) EMM 73-21-01-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Engine Electronic Controller (EEC) EMM 73-21-01-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Removal of the Inter-Turbine Temperature (ITT) Harness EMM 77-21-02-000-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Installation of the Inter-Turbine Temperature (ITT) Harness EMM 77-21-02-400-801 [ Global Express ]  [ G5000 ]  [ Global XRS ]
Wire Repair - Maintenance Practices - ALL SPM 20-12-10-02 [ Global Express ]  [ G5000 ]  [ Global XRS ]

Troubleshooting Recommendations:

CAUTION: DO NOT DO ELECTRICAL CHECKS INTO THE ENGINE ELECTRONIC CONTROLLER (EEC). IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE EEC CAN OCCUR.

  1. Open the circuit breakers that follow:

    System Name Circuit Breaker Name Bus Name
    ENGINE L FADEC CH A BATT
    ENGINE L FADEC CH B BATT
    ENGINE L ENG IGN 1 BATT
    ENGINE L ENG IGN 2 BATT
    ENGINE L ENG FUEL HPSOV BATT
    ENGINE L ENG START A BATT
    ENGINE L ENG START B BATT
    ENGINE L T/R CTL VALVE BATT
    ENGINE L T/R LOWER LOCK BATT
    ENGINE L T/R UPPER LOCK BATT

  2. Perform a deactivation of the thrust reverser and open the cowls.
  3. Remove the applicable bypass-duct access panel and the applicable combustion section fairing.

    1. If the fault message is stored, fault could be intermittent.
    2. If the fault message is not stored, continue with next step.

  4. Examine the interface wiring for damage between the connectors and the terminal blocks that follow:

    • The EEC connector P1047
    • The bypass duct connectors J1032 and P1032
    • The terminal blocks TB2215, TB2216 and the ground connector GC2203
    • The Alumel and Chromel connector posts on the ITT thermocouples
      CAUTION: DO NOT DO ELECTRICAL CHECKS INTO THE ENGINE ELECTRONIC CONTROLLER (EEC). IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE EEC CAN OCCUR.
      NOTE: Look specially for signs of damage adjacent to clip locations.

    1. If there is damage, repair defective wiring as required and go to step 14.
    2. If there is no damage, continue with next step.

  5. Monitor the system to see if the fault message occurs again.

    1. If the fault message is not active, go to step 14.
    2. If the fault message is active, continue with next step.

  6. Perform the fault isolation for the ITT signal.
  7. Disconnect the EEC connector P1044 and the bypass duct connector P1030. Disconnect the interface wiring at the terminal blocks TB2112, TB2113 and at the ground connector GC2103.
  8. Examine the interface wiring and connectors for damage between the connectors and the terminal blocks that follow:

    • The EEC connector P1047
    • The bypass duct connectors J1032 and P1032
    • The terminal blocks TB2215, TB2216 and the ground connector GC2203
    • The Alumel and Chromel connector posts on the ITT thermocouples
      NOTE: Look specially for signs of chafing adjacent to clip locations, condition of connector pins and wiring kink or strain.

    1. If there is no damage, repair defective wiring as required and go to step 14.
    2. If there is damage, continue with next step.

  9. Clean the terminal blocks TB2215, TB2216 and the ground connector GC2203.
  10. Perform wiring checks between TB2215 and Bypass Duct (P1032).

    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.

  11. Perform wiring checks between TB2216 and Bypass Duct (P1032).

    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.

  12. Perform wiring checks between Bypass Duct (J1032) and EEC (P1047).

    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.

  13. Install the applicable combustion section fairing and the applicable bypass-duct access panel.
  14. Close the cowls and perform the activation of the thrust reverser.
  15. Close the circuit breakers that follow:

    System Name Circuit Breaker Name Bus Name
    ENGINE L FADEC CH A BATT
    ENGINE L FADEC CH B BATT
    ENGINE L ENG IGN 1 BATT
    ENGINE L ENG IGN 2 BATT
    ENGINE L ENG FUEL HPSOV BATT
    ENGINE L ENG START A BATT
    ENGINE L ENG START B BATT
    ENGINE L T/R CTL VALVE BATT
    ENGINE L T/R LOWER LOCK BATT
    ENGINE L T/R UPPER LOCK BATT

    1. If the fault message stays active, replace the ITT harness and do close out.
    2. If the fault message stays inactive, continue with next step.

  16. Replace the Left EEC.
  17. Make sure that the primary indication of ITT shows on the EICAS display.
  18. Do close out.
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