NTSB CAROL · Event
Event FTW04LA174
Aircraft involved
Probable cause & findings
The pilot's premature lift-off and his failure to abort the takeoff. Contributing factors were the soft and muddy runway conditions and the unfavorable winds.
Factual narrative
On July 4, 2004, approximately 0930 central daylight time, a Grumman AA-1 single-engine airplane, N6241L, was substantially damaged following a loss of control during takeoff from Cedar Mills Airport (3T0), a turf airstrip, near Gordonville, Texas. The commercial pilot and passenger sustained minor injuries. The airplane was registered to and operated by the pilot. 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, with Hicks Airfield (T67), near Saginaw, Texas, as its intended destination. The 4,333-hour pilot reported in the Pilot/Operator Aircraft Accident Report (NTSB Form 6120.1/2) that there was an "almost direct crosswind," as the airplane departed from runway 07. The down-hill runway is 3,000 feet long and 60 feet wide, and is adjacent to a lake. The pilot further stated that the runway was soft. The pilot elected to use a "soft field" takeoff technique as he expected a longer than normal takeoff roll due to the soft runway condition. The pilot noted that the acceleration was "a bit slower than I was used to, but seemed OK." Approximately halfway down the runway, "the airplane became airborne, with a short squawk from the stall warning system." The pilot "let off some back pressure, and the airplane touched down for a few feet before getting airborne again." As the airplane passed a large tree on the departure end of the runway, the pilot reported that a "gust of wind" caught the right wing, and the nose dipped down. Subsequently, the left wing impacted water and the airplane came to rest in the inverted position in the lake. Examination of the airplane by an Federal Aviation Administration (FAA) inspector, who responded to the accident site, revealed structural damage to both wings and the tail section. The cockpit area, fuselage, propeller, and engine cowling also received substantial damage. At 0950, the automated surface observing system at Grayson County Airport (GYI), near, Sherman/Denison, Texas, located 10 miles southeast from the accident site, reported wind from 210 at 15 knots, visibility 10 statute miles, clouds scattered at 1,700 feet, temperature 82 degrees Fahrenheit, dew point 73 degrees Fahrenheit, and barometric pressure of 29.92 inches of Mercury. The density altitude was calculated by the NTSB investigator-in-charge at 2,333 feet. The 4,333-hour pilot stated that there was an "almost direct crosswind," as the airplane attempted to takeoff from a 3,000 feet long turf runway. The runway was reported to be "soft" and the pilot expected a longer than normal takeoff roll and elected to use the "soft field" takeoff procedure. The pilot further stated that acceleration was "a bit slower than he was used to, but seemed OK." Approximately halfway down the runway, "the airplane became airborne, with a short squawk from the stall warning system." The pilot "let off some back pressure, and the airplane touched down for a few feet before getting airborne again." As the airplane passed a large tree on the departure end of the runway, the pilot reported that a "gust of wind" caught the right win, and the nose dipped down. Subsequently, the left wing impacted water before the airplane came to rest in an inverted position in a lake. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_FTW04LA174.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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