NTSB CAROL · Event
Event BFO95LA080
Aircraft involved
Probable cause & findings
the pilot's delay in aborting the takeoff.
Factual narrative
On August 13, 1995, at 1101 eastern daylight time, a Cessna 182F, N3516U, collided with a fence during an aborted takeoff at Freeway Airport, Mitchellville, Maryland. The certificated private pilot and the three passengers were not injured. The airplane sustained substantial damage. Visual meteorological conditions prevailed and a flight plan was not filed. The personal flight was conducted under 14 CFR 91. The intended destination was Ocean City, Maryland. The pilot reported that as the airplane accelerated on the takeoff roll on runway 36, when he applied back pressure to rotate, the stall warning horn sounded. He stated that he lowered the nose and the airplane settled onto the runway. The pilot stated that he continued the takeoff roll and rotated a second time. The stall warning horn sounded again, so the pilot aborted the takeoff. During the aborted takeoff the airplane touched down hard and the pilot stated that he reduced the power to idle and applied the brakes. The pilot stated that a highway crossed the end of the runway so he swerved the airplane to avoid exiting the runway onto the highway. The airplane collided with tall grass and a fence. The pilot reported that the temperature was 88 degrees Fahrenheit, and there was 43 gallons of fuel on board the airplane. The pilot stated that when he applied back pressure to rotate during the takeoff roll on runway 36, the stall warning horn sounded. He lowered the nose and the airplane settled onto the runway. He continued the takeoff roll and when he rotated a second time the stall warning horn sounded again. He realized that the airplane would not fly so he aborted the takeoff. The airplane bounced and the pilot applied brakes to avoid exiting the runway onto the highway that crossed the end of the runway. He stated that he intentionally swerved the airplane, and the airplane exited the runway and collided with a fence. There were four occupants on board the airplane. The pilot reported that the temperature was 88 degrees Fahrenheit, and there was 43 gallons of fuel on board the airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_BFO95LA080.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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