NTSB CAROL · Event
Event FTW02LA041
Aircraft involved
Probable cause & findings
the pilot's inadvertent stall during takeoff, which resulted in a loss of control and the airplane colliding with a fence and a tree. A contributing factor was his lack of experience in the make and model of aircraft.
Factual narrative
On November 22, 2001, at 1040 central standard time, a Globe GC-1B tail-wheel equipped airplane, N3209K, was substantially damaged when it impacted a fence and a tree during takeoff from the Zuehl Airport, Marion, Texas. The airplane was registered to and operated by the pilot. The private pilot sustained minor injuries and the pilot-rated passenger received serious injuries. Visual meteorological conditions prevailed and a flight plan was not filed for the 14 Code of Federal Regulations Part 91 personal flight. The flight was originating at the time of the accident and was destined for a private airstrip near Eagle Pass, Texas. According to the pilot's written statement, he arrived at the airport, inspected the airplane, added 43 gallons of fuel, and sumped the fuel tanks twice. The pilot taxied to the end of the 3,000-foot grass runway and conducted an engine run-up by applying power to 1,700 rpm, checking the magnetos and carburetor heat, and cycling the propeller. The pilot completed the takeoff checklist and entered the runway for takeoff. As the airplane rolled down the runway, he noticed that the airplane was heading toward the left side of the runway. He applied right rudder to straighten the airplane. The pilot reported that the airplane traveled down the runway "a long way," and he checked that the throttle, propeller, and mixture controls were in the full forward position. The airspeed indicator read 65 mph, and the airplane felt "light on the wheels," so the pilot pulled back on the control stick. The airplane veered to the left toward a building and trees. The pilot added that he "may have stalled the [air]plane," since his passenger reported that the airplane had a "sharp, left wing drop stall." The airplane then impacted and continued through a chain link fence and impacted a tree, where it came to rest upright. The pilot "turned off all switches (fuel pump, master, ignition)" and exited the airplane. The airplane sustained structural damage to its fuselage and wings. According to the pilot, the airplane had not flown in 1.5 years and had undergone an annual inspection on November 20, 2001. According to the Pilot/Operator Aircraft Accident Report, the pilot had never flown this make and model aircraft before and had accumulated a total of 126.2 flight hours. The pilot reported that he had obtained his tail-wheel endorsement in a Citabria 7ECA aircraft on November 9, 2001. Examination of the aircraft and engine by the FAA inspector, who responded to the accident site, revealed no evidence of any anomalies. During the initial takeoff climb from the 3,000-foot grass runway, the airplane veered to the left toward a building and trees. The private pilot stated that he "may have stalled the [air]plane," since his pilot-rated passenger reported that the airplane had a "sharp, left wing drop stall." The airplane then impacted and continued through a chain link fence and impacted a tree. The pilot had not flown this make and model aircraft before and had accumulated a total of 126.2 flight hours. The pilot reported that he had obtained his tail-wheel endorsement 13 days prior to the accident. Examination of the aircraft and engine revealed no evidence of any anomalies. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_FTW02LA041.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, loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Semantic Scholar 2016 · Article (Interacción)
Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report
Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- 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 …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- arXiv 2025 · arXiv preprint
Quadratic Programming Approach to Flight Envelope Protection Using Control Barrier Functions
Ensuring the safe operation of aerospace systems within their prescribed flight envelope is a fundamental requirement for modern flight control systems.
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
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