What was found
PART REJECTED AT FLUORESCENT PENETRANT INSPECTION DUE TO CRACK ON OUTSIDE TOP FLAT, APPROXIMATELY 0.375 INCH IN LENGTH, AS MARKED ON PART.
- Difficulty date
- May 19, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Filed by
- KB1R264K
Fountain Plating Company, LLC - Engine
- Iae V2500A1
- System (JASC)
- 7230 · Turbine Engine Compressor Section
- Part
- Seal
- Part number
- 2A0851
- Condition
- Cracked
- Location
- Engine
- 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.