What was found
(CAN) CRACKS FOUND IN THE BEND RADIUS OF THE SECOND STAGE NOZZLE DIAPHRAGM. NOZZLES SENT TO MANUFACTURER. PART TC: 3,030.
- Difficulty date
- May 22, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Allsn 250C20R2
- System (JASC)
- 7250 · Turbine Section
- Part
- Nozzle
- Part number
- 23031938
- Condition
- Cracked
- Location
- 2nd Stage
- Part time
- 3,499 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.