What was found
PART REJECTED FOR CRACKS IN 2 PLACES. 2 CRACKS ON OUTSIDE DIAMETER WALL IN CLOSE LINEAR ALIGNMENT - 0.060 INCH THICK. CRATER TYPE CRACK IN INSIDE DIAMETER FLANGE, 0.125 INCH DIAMETER. (X)
- Difficulty date
- May 10, 1999
- Submitted
- July 12, 2000
- Operation
- General aviation
- Engine
- Iae V2500A1
- System (JASC)
- 7250 · Turbine Section
- Part
- Bearing
- Part number
- 2A0847
- Condition
- Cracked
- Location
- Od Wall & Id Flg
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.