What was found
(CAN) TORQUE SPLIT OF 2 TO 3 PERCENT BETWEEN THE ENGINES AT HIGH POWER SETTINGS. MAINTENANCE REPLACED NR 1 ENGINE TOTAL INLET TEMPERATURE T 1.8, T1.5, SENSOR. AFTER REVIEW OF EMU DATA.
- Difficulty date
- May 27, 2013
- Submitted
- September 14, 2015
- Operation
- General aviation
- Make and model
- Bombdr DHC8400
- Engine
- Pwc PW150A
- Propeller
- Rotol CR4086123F17
- System (JASC)
- 7720 · Engine Temperature Indicating System
- Part
- Sensor
- Part number
- 307600201
- Condition
- Malfunctioned
- Location
- Nr 1 Tit
- Stage of operation
- CL
- How discovered
- O
- Nature of condition
- N
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.