What was found
(AUS) FUSELAGE RIGHT FORWARD LOWER DOOR POST BULKHEAD CRACKED AT RELIEF HOLE PER AD/CESSNA206/48 AMDT1. CRACK LENGTH 8.2 MM (0.325 INCH). AD/CESSNA206/48 AMDT1 WAS NOT DUE FOR ANOTHER 120 HOURS. (X)
- Difficulty date
- September 28, 2000
- Submitted
- November 2, 2000
- Operation
- General aviation
- Make and model
- Cessna U206G
- Engine
- Cont IO520F
- Propeller
- Mcauly D2A34C58
- System (JASC)
- 5312 · Fuselage Main, Bulkhead
- Part
- Post
- Condition
- Cracked
- Location
- Fuselage Main Bu
- Component
- Fuselage Main Bu
- 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.