What was found
TURBINE DISASSEMBLED DUE TO N1 DRAG ON TEST CELL. UPON INSPECTION OF TURBINE PARTS NOTED: TIP DRAG ON NR 2 NOZZLE 1ST STAGE TIP PATH. INSTALLED AN OVERHAULED NR 2 NOZZLE.
- Difficulty date
- October 31, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Allsn 250C30P
- System (JASC)
- 7250 · Turbine Section
- Part
- Nozzle
- Part number
- 23055438
- Condition
- Failed
- Location
- 2nd Stage
- 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.