What was found
AFTER REMOVAL OF SHIMS TO COMPLY WITH TB 206L-94-169, CRACK WAS FOUND UNDER SHIM AT LEFT LOWER ATTACH POINT. APPARENTLY, A STRESS CRACK CAUSED BY WORKING RIVETS IN INTERCOSTAL ASSEMBLY.
- Difficulty date
- May 31, 1995
- Submitted
- March 26, 2000
- Operation
- General aviation
- Aircraft
- N2092U
- Make and model
- Bell 206L1
- Aircraft serial
- 45697
- System (JASC)
- 5312 · Fuselage Main, Bulkhead
- Part
- Bulkhead
- Part number
- 206032400027S
- Condition
- Cracked
- Location
- Forward On T/B
- Part time
- 7,851 hours
- Component
- 206033004045
- 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.