What was found
(CAN) VERTICAL CONTROL TUNNEL AFT RIGHT STIFFENER CRACKED. BELL TB 206L-79-41 HAD NOT BEEN ACCOMPLISHED.
- Difficulty date
- August 17, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Bell 206L
- Engine
- Allsn 250C20
- System (JASC)
- 5320 · Fuselage Miscellaneous Structure
- Part
- Stiffener
- Part number
- 206033110239
- Condition
- Failed
- Location
- Fuselage
- Part time
- 8,600 hours
- Component
- 206033002005
- 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.