What was found
(CAN) THE LEADING EDGE OF THE COMPRESSOR SCROLL TURNING VANE EXHIBITS A CRACK 1 INCH PARALLEL TO AND .5 INCH FROM THE LEADING EDGE.
- Difficulty date
- August 23, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Allsn 250C47B
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Vane
- Part number
- 23064577
- Condition
- Cracked
- Location
- Compressor
- Part time
- 2,000 hours
- 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.