What was found
ENGINE 1ST STAGE BOOSTER INCOMPLETE WELDED PENETRATION.
- Difficulty date
- August 15, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Ge CFM562
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Booster
- Part number
- 301288147D
- Condition
- Miswelded
- Location
- 1st Stage
- Stage of operation
- IN
- Nature of condition
- W
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.