01/03/25
Message Overview:
Message Description:
Left engine TT2 sensor/heater fault 4.
[MCID 0805]
TT2 Sensor/Heater 4.
Detection of a fault primarily in the TT2 sensor/heater.
Possible Causes:
- Wiring Harness (W1)
- Wiring Harness (W6)
- TT2 Current Sense Relay in the DC Power Center (DCPC)
- TT2 Sensor
Troubleshooting Tips:
Advisory Wire/Service Bulletin: None
Forum Articles/Infoservice/Newsletter: None
- If the L or R ENGINE FAULT CAS message is shown with this fault, this is a No Dispatch condition.
- If there is not a L or R ENGINE FAULT CAS message, only a MCID or fault equation, then this is a Long Term Dispatch (LT) fault and is subject to correction outlined in the Honeywell LEMM SUBTASK 5-10-00-200-003.
- Check for the following MDC messages displayed with the fault: X-channel bus 1A (MCID 0905), X-channel bus 1B (MCID 0906), X-channel discrete 1A (MCID 0933), X-channel discrete 1B (MCID 0934). If any of the above MCID codes are posted, correct the cross channel faults first.
Quick Links:
| Standard Aircraft Configuration for Maintenance | AMM 12-00-00-867-803 |
| Electrical/Electronic Safety Precautions | AMM 24-00-00-910-801 |
| Electrostatic-Discharge Safety Precautions | AMM 24-00-00-910-802 |
| Connect Electrical Power to the Aircraft | AMM 24-00-00-861-801 |
| Remove the Electrical Power from the Aircraft | AMM 24-00-00-861-802 |
| Removal of the DC Power Center (DCPC) | AMM 24-61-01-000-801 |
| Installation of the DC Power Center (DCPC) | AMM 24-61-01-400-801 |
| Functional Test of the DC Power Center (DCPC) | AMM 24-61-01-720-801 |
| Operational Test of the Nacelle Anti-Ice System | AMM 30-21-00-710-801 |
| General Visual Inspection of the Engine Wiring Harness | AMM 71-50-00-210-802 |
Troubleshooting Recommendations:
- Check MDC for faults, if a MCID 805 is listed, troubleshoot using the following steps for aircraft and engine fault isolation with reference to the Light Engine Maintenance Manual Subtask 72-00-00-810-117-A01.
- Make sure Circuit Breaker (CB) CB1-E11 is set to IN.
- Perform the Operational Test of the Nacelle Anti-Ice System (AMM TASK 30-21-00-710-801). View the ANTI-ICE synoptic page, paying attention for the amber T2 fault. Is the fault still present?
- If YES, continue with next step.
- If NO, do close out.
- Perform a continuity/resistance check of the TT2 probe heater. Measure the resistance from the Left DC Power Center A35P3 pin 52 to ground, there should be continuity ≈ 5 to 30 Ω.
- If resistance value is out of tolerance, replace the TT2 sensor.
- If there is no continuity, continue with next step.
- Gain access to the engine connectors listed in the table below. Inspect for proper installation or damage and rectify if required. Perform a wiring check as follows:
From To Value TT2 Sensor Pin 5 TT2 Sensor Pin 6 ≈ 5 to 30 Ω W6P7 Pin 6 Ground <.01 Ω W6P7 Pin 5 A35P3 Pin 52 <.01 Ω - If wiring defects are found, repair defective wiring as required and do close out.
- If no defects are found, continue with next step.
- Perform a continuity check of the TT2 sense output from the Left DC Power Center to the ECU Channel A & B.
From To Value A35P3 Pin 8 W6P3/A41J1 Pin 63 <.01 Ω A35P3 Pin 33 W6P2/A43J2 Pin 63 <.01 Ω - If wiring defects are found, repair defective wiring as required and do close out.
- If no defects are found, continue with next step.
- Replace the DC power center PCB1 protection card.
- Do close out.




