What was found
(AUS) HIGH PRESSURE COMPRESSOR ROTOR SPOOL NR 3 STAGE TO NR 9 STAGE OUTSIDE OF LIMITS AS PER AD/CF6/41, AD/CF6-43, FAA AD FAD 99-24-15 AND FAA AD FAD 2000-16-12.
- Difficulty date
- January 12, 2001
- Submitted
- March 20, 2001
- Operation
- General aviation
- Engine
- Ge CF680C2*
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Turbine Wheel
- Part number
- 9380M28P05
- Condition
- Out Of Tolerance
- Location
- Engine
- Part time
- 32,002 cycles
- Component
- Ge
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.