Probable cause
The failure of the tailwheel to remain locked during a crosswind landing, which resulted in a loss of directional control.
NTSB analysis
The pilot landed the tailwheel-equipped airplane with a crosswind, and during the landing rollout the airplane veered to the right. The pilot's attempts to correct the veer by applying left rudder pedal and left brake were unsuccessful. The airplane exited the right side of the runway, ground looped, and the left main landing gear collapsed resulting in substantial damage to the fuselage. A postaccident examination of the airplane revealed that the tailwheel assembly, tailwheel steering arm, and rudder stops were all in working condition. However, when combined together, the resulting configuration allowed the tailwheel to unlock and fully swivel 15 degrees prior to the rudder reaching full travel in either direction. Subsequently, when the airplane slowed to an airspeed at which the rudder was no longer effective and rudder input was added to correct for the crosswind, the tailwheel disengaged, resulting in the runway excursion.
Text from the NTSB. Open the NTSB docket for CEN11LA658 for the full record.
Event
- Date
- Sep 18, 2011
- Type
- Accident
- Place
- Lancaster, Texas
- Nearest airport
- Lancaster Regional (LNC)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Amateur-built RV-8
- N-number
- N98D
- 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.