09/25/19
Message Overview:
Fault Message:
L ITT SIGNAL CH B RNG
Fault Code:
7325726LBR
Associated CAS:
| 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.
- 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 - Perform a deactivation of the thrust reverser and open the cowls.
- Remove the applicable bypass-duct access panel and the applicable combustion section fairing.
- If the fault message is stored, fault could be intermittent.
- If the fault message is not stored, continue with next step.
- 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.
- If there is damage, repair defective wiring as required and go to step 14.
- If there is no damage, continue with next step.
- Monitor the system to see if the fault message occurs again.
- If the fault message is not active, go to step 14.
- If the fault message is active, continue with next step.
- Perform the fault isolation for the ITT signal.
- 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.
- 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.
- If there is no damage, repair defective wiring as required and go to step 14.
- If there is damage, continue with next step.
- Clean the terminal blocks TB2215, TB2216 and the ground connector GC2203.
- Perform wiring checks between TB2215 and Bypass Duct (P1032).
- If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Perform wiring checks between TB2216 and Bypass Duct (P1032).
- If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Perform wiring checks between Bypass Duct (J1032) and EEC (P1047).
- If wiring checks are not good, repair defective wiring as required and do close out.
- If wiring checks are good, continue with next step.
- Install the applicable combustion section fairing and the applicable bypass-duct access panel.
- Close the cowls and perform the activation of the thrust reverser.
- 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 - If the fault message stays active, replace the ITT harness and do close out.
- If the fault message stays inactive, continue with next step.
- Replace the Left EEC.
- Make sure that the primary indication of ITT shows on the EICAS display.
- Do close out.
