What was found
(CAN) INSPECTION OF STUDS AS PER AWD 95-20-07 REVEALED FINE LINEAR CRACK INDICATIONS AT THE RADIUS UNDER THE BOLT HEAD. THE BOLTS WERE REJECTED.
- Difficulty date
- March 26, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Piper PA24250
- Engine
- Lyc O540A1A
- System (JASC)
- 3211 · Main Landing Gear Attach Section
- Part
- Stud
- Part number
- 2082900
- Condition
- Cracked
- Location
- Mlg
- Part time
- 3,155 hours
- Component
- Piper
- 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.