Probable cause
The improper installation of the rudder cable to rudder pedal attachment hardware.
NTSB analysis
Prior to the flight, the pilot performed a preflight inspection, but he did not inspect the rudder pedals and rudder cable attachments. During takeoff, approximately 50 feet above ground level, the pilot felt something unusual with the left rudder pedal. The airplane immediately veered to the right, and the pilot initiated a climb in an attempt to troubleshoot the problem. Unable to determine what happened, the pilot maneuvered the airplane back to the airport. The airplane was difficult to control to the left and he determined he had to make a landing on the grass adjacent to the runway. During the landing, the airplane impacted a drainage ditch. The airplane sustained substantial damage to the firewall. Postaccident examination of the airplane revealed the bolt/nut hardware that connected the left rudder cable to the rudder pedal had separated, and the cable became disconnected from the pedal. The nut, which is to be secured by a cotter pin, backed off of the bolt. The bolt and nut were found within the airplane. The experimental amateur-built airplane had accumulated approximately 19 hours of flight time, at the time of the accident.
Text from the NTSB. Open the NTSB docket for CEN11CA282 for the full record.
Event
- Date
- Apr 12, 2011
- Type
- Accident
- Place
- Davenport, Iowa
- Nearest airport
- Davenport Municipal Airport (DVN)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Amateur-built ZENITH CH-701
- N-number
- N701YB
- Category
- Airplane
- Damage
- Substantial
- Operating rule
- Part 91 (general aviation)
- Purpose of flight
- Personal
From the NTSB aviation accident database: N-registered aircraft, events since 2008, data through Oct 28, 2026. The file is published monthly, so the latest weeks are incomplete and recent records can change. The official source is the NTSB aviation investigation search. CheckAero is independent and not affiliated with the NTSB.