NTSB CAROL · Event
Event MIA07CA139
Registry · N84GT
FAA Aircraft Registry record.
Make / Model
SOCATA TB-20 TRINIDAD
Year of manufacture
2001 · 6 years old at event
Engine
LYCOMING IO-540 SER (300 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
20010712
ADS-B equipped
Yes — Mode-S AB7E28
Registrant of record
DODSON INTERNATIONAL PARTS INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to obtain adequate airspeed for takeoff which resulted in a stall, runway overrun down an embankment, and collision with a fence. A factor in accident was the pilot not utilizing the full length of the runway for takeoff.
Factual narrative
The pilot stated to a New York State Police Officer that while attempting to takeoff from the runway his aircraft began to stall and therefore he tried to abort his takeoff; however, he was not able to fully abort and slid off the runway and impacted a fence before coming to a stop. Witnesses stated that they observed the airplane enter runway 29 at intersection H. Shortly after, the airplane was seen porpoising toward the end of the runway before it skidded off the end of the runway and down an embankment. Runway 29 is 4,451 x 150 foot long and intersection H is located about one third down the runway. A completed Pilot/Operator Aircraft Accident /Incident Report (NTSB form 6120.1/2) was not received for this accident. The pilot stated to a New York State Police Officer that while attempting to takeoff from the runway his aircraft began to stall and therefore he tried to abort his takeoff; however, he was not able to fully abort and slid off the runway and impacted a fence before coming to a stop. Witnesses stated that they observed the airplane enter runway 29 at intersection H. Shortly after, the airplane was seen porpoising toward the end of the runway before it skidded off the end of the runway and down an embankment. Runway 29 is 4,451 x 150 foot long and intersection H is located about one third down the runway. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_MIA07CA139.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 ↗