NTSB CAROL · Event
Event CEN12LA304
Registry · N68543
FAA Aircraft Registry record.
Make / Model
BELLANCA 7GCAA
Year of manufacture
1972 · 40 years old at event
Engine
LYCOMING 0-320 SERIES (180 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19720901
ADS-B equipped
Yes — Mode-S A918CA
Registrant of record
WALTEMATH TROY A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's loss of directional control during landing, which resulted in a runway excursion.
Factual narrative
On May 14, 2012, about 1630 central daylight time, a Bellanca 7GCAA, N68543, went off the right side of runway 15 and impacted a ditch at Captain Jack Thomas Airport (KEQA), El Dorado, Kansas. The pilot and passenger were not injured. The airplane was substantially damaged. The airplane was registered to and operated by a private individual under the provisions of 14 Code of Federal Regulations (CFR) Part 91 as a personal flight. Visual meteorological conditions (VMC) prevailed at the time of the accident, and no flight plan had been filed. The flight originated from Benton (K1K1), Kansas, about 1545. The pilot said he was making a full-stall landing to the south with an east to west wind. Upon touchdown, he lost directional control and the airplane went off the right side of the runway and into a deep ditch. The right main landing gear separated from the airframe, and the right wing was damaged when it struck the embankment. The pilot reported no mechanical discrepancies with the airplane prior to the accident. His recommendation for preventing this accident was for him to receive additional training in the airplane and acquire more proficiency. Although he indicated he had logged 1,900 total hours and 600 hours in single-engine airplanes, he had only 1 hour in the Bellanca 7GCAA. An examination of the airplane and related systems revealed no anomalies. The pilot reported that he made a full-stall landing on the runway with a left crosswind and lost directional control after landing. The airplane departed the right side of the runway and impacted a deep ditch. The pilot reported no preimpact mechanical malfunctions or failures that would have precluded normal operations. 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 Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2012_CEN12LA304.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, runway excursion). 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 …
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Runway Excursion — SKYbrary Knowledge Base
SKYbrary runway excursion review — RE-OE (overruns) + RE-LO (lateral). Risk drivers: long landing, high approach speed, contaminated surface, tailwind, mis-set autobrakes.
- 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
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…
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