NTSB CAROL · Event
Event MIA06LA127
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airspeed while maneuvering which resulted in a stall.
Factual narrative
On August 11, 2006, about 2000 eastern daylight time, N9898B, an American Champion 7EC, registered to and operated by Seminole Aviation Association Inc., as a Title 14 CFR Part 91 personal flight, crashed while the pilot was maneuvering following takeoff at Manatee Airport, Palmetto, Florida. Visual meteorological conditions prevailed, and no flight plan was filed. The airline-rated pilot received minor injuries, and the airplane incurred substantial damage. The flight was originating at the time of the accident. The pilot stated that he took off from runway 7, at Manatee Airport, performed a climbing right turn to make a 45-degree heading change to the right, and upon reaching 200 feet altitude initiated a descending left turn to 225 degrees, in an effort to reverse course and fly along runway 25. According to the pilot, in the turn the airplane became unresponsive about the roll axis, and the airplane continued the descent in a nose low, left wing low attitude. He said he applied full right aileron, full up elevator, and full right rudder control inputs, but was unable to arrest the rate of descent. The airplane impacted the ground in a slight left wing low nose low attitude. On August 12, 2006, an FAA inspector conducted a post accident examination of the airplane, and no preaccident anomalies were noted to exist. The pilot stated that he took off from runway 7, at Manatee Airport, performed a climbing right turn to make a 45-degree heading change to the right, and upon reaching 200 feet altitude initiated a descending left turn to 225 degrees, in an effort to reverse course and fly along runway 25. According to the pilot, in the turn the airplane became unresponsive about the roll axis, and the airplane continued the descent in a nose low, left wing low attitude. He said he applied full right aileron, full up elevator, and full right rudder control inputs, but was unable to arrest the rate of descent. The airplane impacted the ground in a slight left wing low nose low attitude. On August 12, 2006, an FAA inspector conducted a post accident examination of the airplane, and no preaccident anomalies were noted to exist. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_MIA06LA127.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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