NTSB CAROL · Event
Event NYC01LA011
Registry · N1066M
FAA Aircraft Registry record.
Make / Model
BOEING B75N1
Year of manufacture
1942 · 58 years old at event
Engine
CONT MOTOR W670 SERIES (250 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19650114
ADS-B equipped
Yes — Mode-S A01E34
Registrant of record
N1066M LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper recovery from a bounced landing.
Factual narrative
On October 7, 2000, about 1430 Eastern Daylight Time, a Boeing B75-N1 Stearman, N1066M, was substantially damaged while landing at the Flying Circus Aerodrome Airport (3VA3), Warrenton, Virginia. The certificated private pilot was not injured. Visual meteorological conditions prevailed and no flight plan had been filed for the local personal flight that was conducted under 14 CFR Part 91. According to the pilot, he departed 3VA3, and flew to the Culpeper Regional Airport (CJR), Culpeper, Virginia, to perform a "fly-over and balloon-bust" as part of an air show. He then returned to 3VA3 for landing. The airplane was landing on Runway 34, a 2,500 foot-long, 150 foot-wide, turf runway. The pilot stated that after he observed two other airplanes land, he noted the winds were from the northwest, and elected to perform a "wheel landing," instead of the "normal 3-pt, stall landing." After touchdown, the airplane bounced twice on its main landing gear, and then suddenly pitched over. The pilot further stated "I believe I had inadvertently slid my feet too high on the rudder pedals and hit the brakes on the second bounce. The pilot also stated he did not experience any mechanical problems with the airplane. The pilot reported 872 hours of total flight experience, which included 600 hours accumulated in tail-wheeled airplanes, and 105 hours in the make and model of the accident airplane. The wind reported at CJR, which was located about 8 miles, west-southwest of the accident site, at 1422, was from 350 degrees at 6 knots. During touchdown, the airplane bounced twice on its main landing gear, and then suddenly pitched over. The pilot stated 'I believe I had inadvertently slid my feet too high on the rudder pedals and hit the brakes on the second bounce. The pilot also stated he did not experience any mechanical problems with the airplane. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_NYC01LA011.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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