NTSB CAROL · Event
Event ATL00LA064
Aircraft involved
Probable cause & findings
The pilot's failure to maintain airspeed during final approach to landing, resulting in an inadvertent stall.
Factual narrative
On June 10, 2000, about 1900 eastern daylight time, an Aeronca 7BCM, N83972, registered Seminole Aviation Association, Inc., was substantially damaged when it collided with the ground during landing flare/touchdown to runway 7 at Manatee Airport in Palmetto, Florida. The commercial pilot received serious injuries and one passenger received minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight being conducted under Title 14 CFR Part 91. The flight originated from Vandenberg Airport in Tampa, Florida, at 1730. According to the pilot, he was practicing a power-off landing on runway 7. He stated that while on the downwind leg at 600 feet above ground level (agl), he applied carburetor heat and retarded the throttle to idle. After turning final, he attempted to "bring back power," but there was "no response." The airplane impacted the north side of the midfield point of the runway in a wings level attitude. The propeller was damaged, and the right wing was bent down 30 degrees. However, according to one witness, he observed the airplane on a "close-in" right downwind, and heard the engine's power reduced to idle. He stated that at the time, the airplane's altitude was 300 to 500 feet agl. Shortly thereafter, the airplane "banked sharply into a right base" at the midpoint of the runway. He stated that "in lining up the aircraft for final approach, the bank was held for most of the base leg and appeared to increase to avoid overshooting the runway. Altitude quickly decreased as the aircraft turned and [the] engine stayed at idle speed. At approximately 40 to 60 feet agl, the wings were leveled and the engine surged briefly. Forward airspeed had almost completely dissipated." The airplane then impacted hard on the runway. Another witness stated that he observed the pilot make a "steep turn to base," then banked the airplane "very steep to make the runway" onto final approach. During the bank, the airplane lost altitude and the pilot "tried to add power prior to impact." According to an FAA inspector, a postaccident examination of the airplane revealed no mechanical discrepancies. Weather conditions at the time of the accident were not favorable for the formation of carburetor ice. The pilot was practicing a power-off landing on runway 7. While on the downwind leg of the traffic pattern, he retarded the throttle to idle. Shortly after turning onto final approach, he stated that he attempted to apply power but there was 'no response.' However, witnesses observed the pilot turn the airplane onto the base leg in a steep right bank at the midpoint of the runway. The steep bank continued while the airplane turned onto final approach, and the airplane descended rapidly. At 40 to 60 ft. agl, the wings were leveled while the airplane had diminutive forward airspeed. Both witnesses heard what sounded like power being applied to the engine moments before impact. The airplane then impacted the ground near the midfield point of the runway in a wings level attitude, damaging the propeller and right wing. A postaccident examination of the airplane revealed no mechanical discrepancies, and weather conditions at the time of the accident were not favorable for the formation of carburetor ice. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_ATL00LA064.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 (icing, 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.
- 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 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…
- NASA NTRS 2019 · Contractor Report (CR)
An Evaluation of an Analytical Simulation of an Airplane with Tailplane Icing by Comparison to Flight Data
This report presents the assessment of an analytical tool developed as part of the NASA/FAA Tailplane Icing Program. The analytical tool is a specialized simulation program called TAILSM4 which was de…
- NASA NTRS 2019 · Technical Publication (TP)
NASA/FAA Tailplane Icing Program: Flight Test Report
This report presents results from research flights that explored the characteristics of an ice-contaminated tailplane using various simulated ice shapes attached to the leading edge of the horizontal …
- NASA NTRS 2019 · Other
[Tail Plane Icing]
The Aviation Safety Program initiated by NASA in 1997 has put greater emphasis in safety related research activities. Ice-contaminated-tailplane stall (ICTS) has been identified by the NASA Lewis Icin…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA)
Airport Policing in Pakistan: Structure, Training, and Issue
Airports are strategically and economically important installations of any country. Airports are the gateway of any country and any incidents at these gateways may harm the very aspects of a country i…
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