Probable cause
Failure of the tailwheel steering assembly during maneuvering flight, which resulted in a loss of directional control during the landing roll.
NTSB analysis
The pilot/builder of the experimental amateur-built, tailwheel-equipped airplane had just completed a flight as part of phase one flight testing. He reported an uneventful approach to landing, with the main landing gear touching down first. However, as soon as the tailwheel made contact with the runway, the airplane yawed violently to the right. The pilot applied full left rudder and brake control input, but the airplane did not respond, and departed the runway descending down an embankment. The airplane sustained substantial damage to the upper wing spar and fuselage structure at the landing gear attach points.
Postaccident examination revealed that the tailwheel was locked 90 degrees to the right. The tailwheel assembly was disassembled, and the steering arm cam spring appeared jammed between the shaft and housing. The inner surface of the housing exhibited scoring marks, consistent with a pre-existing failure of the spring. The pilot reported that he had purchased the tailwheel assembly used, and that he did not have any records indicating its manufacturer or serial number.
Text from the NTSB. Open the NTSB docket for WPR14CA390 for the full record.
Event
- Date
- Sep 25, 2014
- Type
- Accident
- Place
- Sedona, Arizona
- Nearest airport
- Sedona (SEZ)
- Highest injury
- None
- Weather
- Visual (VMC)
- Light
- Day
Amateur-built PITTS S1S
- N-number
- N93DB
- Category
- Airplane
- Year built
- 2013
- 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.