NTSB CAROL · Event
Event MIA95LA176
Aircraft involved
Probable cause & findings
THE PILOT-IN-COMMAND'S INABILITY TO MAINTAIN AIRSPEED AFTER ENCOUNTERING A SUDDEN WIND SHIFT AFTER LIFT OFF RESULTING IN AN INADVERTENT STALL, UNCONTROLLED DESCENT, AND GROUND COLLISION.
Factual narrative
On July 6, 1995, about 1500 eastern daylight time, a Kashpureff Nieuport II, N2175L, registered to the pilot, landed hard when control was lost during takeoff from Venice Municipal Airport, Venice, Florida, while on a 14 CFR Part 91 personal flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft received substantial damage and the commercial-rated pilot was not injured. The flight was originating at the time of the accident. The pilot stated that while climbing through 25 feet agl after takeoff the wind shifted and the aircraft stopped flying. The aircraft descended and landed hard in the turf adjacent to the runway. Automated weather observing system data from the Venice Municipal Airport showed a wind shift from the northeast to the north occurred about the time of the accident. WHILE CLIMBING THROUGH 25 FEET AFTER TAKEOFF THE WIND SHIFTED. THE AIRCRAFT LOST AIRSPEED, STALLED, AND DESCENDED UNCONTROLLED TO GROUND IMPACT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_MIA95LA176.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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