NTSB CAROL · Event
Event CEN12CA607
Aircraft involved
Probable cause & findings
An unlocking of the excessively worn tailwheel lock mechanism, which resulted in a loss of directional control during landing.
Factual narrative
Immediately after liftoff the flight instructor simulated an engine failure and the pilot executed a rejected takeoff, landing on the runway remaining. When the tailwheel contacted the runway it began to "shimmy violently and disengaged the steering pin." The airplane veered to the left and the pilot was unable to stop the veer using right rudder and brake. The airplane exited the left side of the runway moving sideways to the right. The right main landing gear collapsed causing substantial damage to the right wing. An examination of the tailwheel mechanism showed excessive wear in both the locking collar hole and the drag links in the tailwheel assembly. Both pilots stated that they had locked the mechanism before takeoff and had good directional control of the airplane during the takeoff run. Immediately after liftoff, the flight instructor simulated an engine failure, and the pilot executed a rejected takeoff, landing on the remaining runway. When the tailwheel contacted the runway, it began to "shimmy violently and disengaged the steering pin." The airplane veered to the left, and the pilot was unable to stop the veer using the right rudder and brake. The airplane exited the left side of the runway while moving sideways to the right. The right main landing gear collapsed, resulting in substantial damage to the right wing. An examination of the tailwheel mechanism showed excessive wear in both the locking collar hole and the drag links in the tailwheel assembly. It was likely that the locking pin had become retracted from the locking collar on the tailwheel at some time during the takeoff or during the landing. Both pilots stated that they had locked the mechanism before takeoff and had good directional control of the airplane during the takeoff run. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Aircraft-Aircraft systems-Landing gear system-Nose/tail landing gear-Damaged/degraded - C
- C Aircraft-Aircraft systems-Landing gear system-Landing gear steering system-Inoperative - C
Verbatim from NTSB's published report. Source file
NTSB_2012_CEN12CA607.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
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