What was found
FLAP FOLLOW-UP CABLE WAS DISCOVERED CORRODED AND BROKEN IN HALF DURING AN INSPECTION.
- Difficulty date
- July 15, 2005
- Submitted
- July 15, 2005
- Operation
- General aviation
- Aircraft
- N746TA
- Make and model
- Beech 400A
- Aircraft serial
- RK146
- Aircraft time
- 6,580 hours, 5,126 cycles
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Cable
- Part number
- 45A6103511
- Condition
- Broken
- Location
- Zone 500
- Part time
- 6,580 hours, 5,126 cycles
- Stage of operation
- IN
- How discovered
- C
- Nature of condition
- L
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.