NTSB CAROL · Event
Event FTW93LA195
Registry · N116RA
FAA Aircraft Registry record.
Make / Model
AMERICAN CHAMPION AIRCRAFT 7EC
Year of manufacture
2008
Engine
CONT MOTOR O-200A (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20080711
ADS-B equipped
Yes — Mode-S A043F5
Registrant of record
PRESTON WILLIAM A
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE PILOT'S OPERATION OF THE AIRPLANE BEYOND ITS TAKEOFF PERFORMANCE LIMITATIONS AND INADVERTENT STALL. A FACTOR WAS HIGH DENSITY ALTITUDE.
Factual narrative
On June 23, 1993, at approximately 1630 central daylight time, a WSK PXL MIELEC, M-18A Dromader, N116RA, sustained substantial damage when the airplane impacted the terrain during takeoff from a private airstrip near Wheatley, Arkansas. The commercial pilot did not sustain injuries. Visual meteorological conditions prevailed for the local aerial application flight. During a telephone interview, conducted by the investigator in charge with the pilot, the following information was revealed. The pilot had been operating the airplane with the same load weights from the grass airstrip throughout the day. During the day, the temperature and winds increased. The pilot reported the winds from the south southeast at 5 knots and gusty with a temperature of 92 degrees Fahrenheit and a high humidity. The pilot further stated that as the airplane reached the end of the runway, he started dumping the load and pulled the airplane off the ground. As the airplane settled and the left wing hit the ground, the left main gear separated from the airframe and the airplane spun around approximately 180 degrees and slid to a stop. The private agricultural airport elevation was 230 feet MSL. Density altitude was approximately 2,200 feet MSL. On the recommendations section of the enclosed pilot report. NTSB Form 6120.1/2, the pilot entered "longer strip or lower tmperature." DURING THE TAKEOFF ROLL, AS THE AIRPLANE REACHED THE END OF THE AIRSTRIP, THE PILOT DUMPED THE LOAD AND ATTEMPTED TO CLIMB. THE LEFT WING STRUCK THE GROUND AND THE AIRPLANE SETTLED TO THE TERRAIN COLLAPSING THE LEFT MAIN LANDING GEAR. THE PILOT HAD BEEN OPERATING AT THE SAME WEIGHTS FROM THE AIRSTRIP ALL DAY. DURING THE DAY, TEMPERATURE INCREASED. FIELD ELEVATION AND DENSITY ALTITUDE WERE 230 AND 2,200 FEET MSL RESPECTIVELY. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1993_FTW93LA195.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…
Browse the full corpus — academia portal ↗