NTSB CAROL · Event
Event MIA00LA239
Aircraft involved
Probable cause & findings
The student pilot's failure to maintain airspeed on final approach resulting in an inadvertent stall/spin and subsequent in-flight collision with terrain.
Factual narrative
On August 16, 2000, at about 1403 eastern daylight time, a Schweizer SGS 1-34, N7679, registered to Tampa Bay Soaring Society Inc., operating as a 14 CFR Part 91 personal flight, crashed on landing in the vicinity of Zephyrhills Municipal Airport (ZPH), Zephyrhills, Florida. Visual meteorological conditions prevailed, and no flight plan was filed. The glider sustained substantial damage and the student pilot sustained serious injuries. The flight originated from ZPH, about 33 minutes before the accident. The pilot remembers departing on the glider flight; and remembers returning to the traffic pattern, but has no further recall of the events leading up to the accident. The brother of the injured pilot stated he observed the glider established on a low and slow final to runway 36, before the glider started spinning to the right. He contacted UNICOM on a handheld radio and asked them to call 911. The glider was observed to enter the traffic pattern for landing. On final approach the witness described the approach as low and slow, before the glider started spinning to the right and collided with the terrain. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_MIA00LA239.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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