What was found
THE ENGINE HAD A N2 COMPRESSOR FAILURE. ALL REMAINING BLADES, STAGES 14 THROUGH 16, ARE SCRAP INCLUDING A SET OF 130 EACH T-1 BLADES; ALSO, STATORS FROM 13TH THROUGH 16TH ARE SCRAP DUE TO THE C-14 BLADE FAILURE UNKNOWN.
- Difficulty date
- January 31, 1995
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Pwa JT3D3B
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Disk
- Part number
- C14
- Condition
- Blade Failure
- Location
- N2 Comp
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.