What was found
BOTH INBOARD FLAP(C3CF104-5) TUBE END ASSEMBLIES (LT AND RT WINGS) C3CF107-3 WERE REPLACED DUE TO WEAR AND LOOSE ATTACH FASTENERS. FAILURE OF THE PLUG END ON THE FLAP CONTROL TUBE COULD LEAD TO AN ASYMMETRIC FLAP CONDITION.
- Difficulty date
- February 9, 2006
- Submitted
- June 6, 2006
- Operation
- General aviation
- Make and model
- Dhav DHC3
- Aircraft time
- 23,363 hours
- Engine
- Pwa R134059
- Propeller
- Hamstd 23D40
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Fitting
- Part number
- C3CF1073
- Condition
- Worn
- Location
- T/E Flap
- Part time
- 23,509 hours
- 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.