NTSB CAROL · Event
Event DEN02LA038
Registry · N624BC
FAA Aircraft Registry record.
Make / Model
CESSNA T337D
Engine
CONT MOTOR IO 520 SERIES (285 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
19690210
ADS-B equipped
Yes — Mode-S A82535
Registrant of record
BAUGH JEFF G
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's misjudged landing flare, which resulted in an inadvertent stall/mush and a hard landing.
Factual narrative
On March 14, 2002, at 1800 mountain daylight time, a Cessna T337D, N624BC, piloted by a private pilot, was substantially damaged during a hard landing on runway 34 (6,606 feet by 100 feet, dry asphalt) at the St. George Municipal Airport, St. George, Utah. Visual meteorological conditions prevailed at the time of the accident. The personal flight was operating under the provisions of Title 14 Code of Federal Regulations Part 91 without a flight plan. The pilot reported no injuries. The cross-country flight originated at Las Vegas, Nevada, at 1659, and was en route to St. George, Utah. A witness to the accident reported that he watched the airplane begin a flare at approximately 50 feet above the runway. The witness said the airplane was going slow. The airplane dropped and struck the runway. A post-accident examination of the airplane by the Federal Aviation Administration showed that the wheel boxes to the main landing gear and the support ribs were bent up and inward. Both blade tips to the aft propeller were curled. The front engine mount was bent. The bottom of the right vertical fin was scraped. The wing section between the fuselage and the right tail boom showed wrinkling. The cargo pod beneath the airplane's fuselage was crushed upward and splintered along both sides. Flight control continuity was confirmed. An examination of the engines, engines controls, and other airplane systems revealed no anomalies. Repeated attempts to obtain a completed Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) from the pilot were unsuccessful. A witness reported seeing the airplane begin a flare at approximately 50 feet above the runway. The witness said the airplane was going slow. The airplane dropped and struck the runway. A post-accident examination of the airplane revealed no evidence of pre-impact anomalies. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_DEN02LA038.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). 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
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…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
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