What was found
(CAN) FUSELAGE SKIN CRACK IN PRESSURE VESSEL LOCATED AT WING TO FUSELAGE FILLET MOUNTING SCREW HOLE (ANCHOR NUT) AT LEFT HAND WING LEADING EDGE (APPROX 1.25 INCHES LONG).
- Difficulty date
- August 15, 2000
- Submitted
- August 30, 2000
- Operation
- General aviation
- Make and model
- Beech 200BEECH
- Aircraft time
- 13,477 hours
- Engine
- Pwa PT6A41
- System (JASC)
- 5300 · Fuselage Structure (General)
- Part
- Skin
- Condition
- Cracked
- Location
- Left Wing
- Part time
- 13,697 hours, 11,735 cycles
- Component
- Fuselage Aerodyn · Beech
- 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.