What was found
(AUS) ENGINE HIGH PRESSURE TURBINE STAGE TWO NOZZLE SEGMENTS (2OFF) SEVERELY CRACKED.
- Difficulty date
- September 3, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Ge CF680A
- System (JASC)
- 7250 · Turbine Section
- Part
- Nozzle
- Part number
- 9234M90G17
- Condition
- Cracked
- Location
- Turbine Section
- 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.