NTSB CAROL · Event
Event MIA96LA228
Aircraft involved
Probable cause & findings
failure of the pilot to extend the wing flaps for takeoff, and his failure to attain sufficient airspeed for flight with the flaps retracted, which resulted in a stall/mush after lift-off.
Factual narrative
On September 7, 1996, about 0940 eastern daylight time, a Canadair T-33, N99195, registered to an individual, collided with terrain during an aborted takeoff, at Charlotte County Airport, Punta Gorda, Florida, while on a Title 14 CFR Part 91 ferry flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft received substantial damage and the airline transport-rated pilot received minor injuries. The flight was originating at the time of the accident. The pilot stated to NTSB that he was ferrying the airplane to Orlando, Florida, for an annual inspection. During the takeoff the aircraft was performing acceptably for flight. After takeoff, the aircraft began to mush and he "knew that it was losing power." He performed an emergency landing straight ahead and after the aircraft came to a stop he exited the aircraft. The pilot stated to an FAA inspector shortly after the accident that the engine developed 100 percent power during the takeoff. He did not report having a loss of engine power. He stated that after the aircraft came to rest, he exited through the broken canopy. The engine continued to run and started a fire in the marsh around the aircraft. He also stated to the FAA inspector that he did not use wing flaps for takeoff. Checklists that were found in the aircraft by an FAA inspector called for wing flaps to be set to 32 degrees for takeoff. A review of the aircraft flight manual by an FAA inspector showed that there are no performance charts for taking off with the wing flaps retracted. (See attached FAA inspector statement and checklists) After takeoff, the aircraft began to mush and would not accelerate. The pilot landed straight ahead in a field. After the aircraft came to rest, the pilot exited the aircraft, and the engine continued to run, causing a fire in the field. The pilot reported to an FAA inspector that the engine developed 100 percent power for takeoff and that he did not use wing flaps for takeoff. The checklist, which was found in the aircraft, required that wing flaps be set to 32 degrees for takeoff. A review of the aircraft flight manual showed that there were no performance charts for taking off with the wing flaps retracted. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_MIA96LA228.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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