What was found
THE FLIGHT CREW ABORTED TAKEOFF ROLL. THE FLIGHT CREW NOTICED ON TAKEOFF ROLL THAT THE RUDDER PEDALS FELT STIFF AND HAD VERY LITTLE MOVEMENT. MAINTENANCE INSPECTED AIRCRAFT RUDDER CONTROL CABLE SYSTEM AND FOUND NO DEFECTS. (K)
- Difficulty date
- November 1, 2005
- Submitted
- February 1, 2006
- Operation
- Air carrier
- Aircraft
- N233CA
- Make and model
- Lear 25B
- Aircraft serial
- 133
- Engine
- Ge CJ6106
- System (JASC)
- 2720 · Rudder Control System
- Part
- Rudder Pedal
- Condition
- Stiff
- Location
- Cockpit
- Stage of operation
- TO
- How discovered
- C
- Nature of condition
- N
- Precautionary procedure
- C
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.