What was found
(CAN) DURING INSPECTION IT WAS DICOVERED THAT THESE CABLES (2EA. 1 LT AND 1 RT) WERE FRAYED WHERE THE CABLE BENDS AROUND THE FLAP CABLE QUADRANT LOCATED IN THE WING TRAILING EDGE.
- Difficulty date
- January 21, 2004
- Submitted
- March 1, 2004
- Operation
- General aviation
- Make and model
- Cessna T337G
- Aircraft time
- 3,465 hours
- Engine
- Cont TSIO360CB
- Propeller
- Mcauly D2AF34C303
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Control Cable
- Part number
- 14601008
- Condition
- Frayed
- Location
- Te Flaps
- 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.