What was found
(AUS) FLAP FOLLOW-UP CABLE DAMAGED. UPLIMIT SWITCH OUT OF ADJUSTMENT. SECONDARY DAMAGE CAUSED BY FLAP OVER-RUN DUE TO THE UPLIMIT SWITCH INCORRECT ADJUSTMENT. (X)
- Difficulty date
- November 3, 2000
- Submitted
- December 7, 2000
- Operation
- General aviation
- Make and model
- Cessna 402B
- Engine
- Cont TSIO520E
- Propeller
- Mcauly 3AF32C87
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Control Cable
- Part number
- 51152242
- Condition
- Failed
- Location
- Te Flap Control
- Component
- Te Flap Control
- Stage of operation
- LD
- How discovered
- V
- Nature of condition
- F
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.