What was found
(CAN) WHILE DOING AD CF-81-25R5, NDT TEST SHOWED A SMALL CRACK IN THE RADIUS OF THE BOLT HEAD. IT IS POSSIBLE THAT CRACK IS OVERLAP OF CAD PLATING.
- Difficulty date
- December 8, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Beech A100
- Engine
- Pwa PT6A28
- System (JASC)
- 5740 · Wing, Attach Fittings
- Part
- Bolt
- Part number
- 8278414
- Condition
- Cracked
- Location
- Wing
- Part time
- 789 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.