What was found
LEFT ENGINE TORQUE FLUX. INSPECTED BLEED VALVE AND BLENDED 1ST STAGE COMPRESSOR BLADES. COULD NOT DUPLICATE. TORQUE FLUX.
- Difficulty date
- January 15, 2002
- Submitted
- February 11, 2002
- Operation
- Air carrier
- Aircraft
- N201GL
- Make and model
- Beech 1900D
- Aircraft serial
- UE201
- Aircraft time
- 13,142 hours, 16,686 cycles
- Engine
- Pwa PT6A67D
- System (JASC)
- 7200 · Engine (Turbine/Turboprop)
- Part
- Engine
- Condition
- Fluctuates
- Location
- Left
- Stage of operation
- CR
- How discovered
- O
- Nature of condition
- O
- Precautionary procedure
- A
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.