What was found
(CAN) DURING A 100 HR INSPECTION THE FLAP CONTROL SYSTEM CENTER CABLE WAS DISCOVERED TO BE FRAYED AT THE AREA OF THE PULLEY. THE CABLE WAS REPLACED NEW.
- Difficulty date
- June 23, 2005
- Submitted
- September 1, 2005
- Operation
- General aviation
- Make and model
- Moravn Z242L
- Aircraft time
- 6,314 hours
- Engine
- Lyc AEIO360A1B6
- Propeller
- Muhbr MTV9*
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Control Cable
- Part number
- Z4243130000
- Condition
- Frayed
- Location
- Te Flap
- 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.