NTSB CAROL · Event
Event WPR13CA261
Registry · N650VX
FAA Aircraft Registry record.
Make / Model
BEECH A23-24
Year of manufacture
1967 · 46 years old at event
Engine
LYCOMING I0360 SER (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20050406
ADS-B equipped
Yes — Mode-S A88EAB
Registrant of record
ONEAL TIMOTHY JAMES
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot’s failure to maintain airplane control and the flight instructors failure to monitor the pilot during a simulated emergency landing.
Factual narrative
The pilot reported that while flying with a certified flight instructor (CFI) for his biannual review, they were simulating an engine failure over the airport with the intent to land on the runway. After spiraling to traffic pattern altitude, the pilot entered a downwind leg for the runway. The pilot turned towards the runway and inadvertently stalled the airplane about 200 feet above the ground. The CFI took over the flight controls; the airplane struck the ground hard, broke off the right main landing gear, and bounced back into the air. The CFI climbed to a safe altitude and circled above the airport before conducting an uneventful landing onto the grass next to the runway. During the accident sequence, the right wing sustained substantial damage. The pilot reported no mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. The pilot reported that while flying with a certified flight instructor (CFI) for his biannual review, they were simulating an engine failure over the airport with the intent to land on the runway. After spiraling to traffic pattern altitude, the pilot entered a downwind leg for the runway. The pilot turned towards the runway and inadvertently stalled the airplane about 200 feet above the ground. The CFI took over the flight controls; the airplane struck the ground hard, broke off the right main landing gear, and bounced back into the air. The CFI climbed to a safe altitude and circled above the airport before conducting an uneventful landing onto the grass next to the runway. During the accident sequence, the right wing sustained substantial damage. The pilot reported no mechanical failures or malfunctions with the airframe or engine that would have precluded normal operation. 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 Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Personnel issues-Psychological-Attention/monitoring-Monitoring other person-Instructor/check pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2013_WPR13CA261.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 (stall, 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.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- 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…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
Browse the full corpus — academia portal ↗