NTSB CAROL · Event
Event NYC96LA140
Aircraft involved
Probable cause & findings
failure of the pilot to maintain control of the glider while being towed during takeoff, which resulted in a pitch oscillation, failure of the tow cable, loss of airspeed, an inadvertent stall/spin, and an uncontrolled collision with the ground.
Factual narrative
On July 5, 1995, about 1315 eastern daylight time, a Schweizer 1-26E glider, N603MX, struck the ground after takeoff from the Marston Mills Airport, Marston Mills, Massachusetts. The private pilot was fatally injured, and the glider was destroyed. Visual meteorological conditions prevailed, and no flight plan had been filed for the local flight which was operated under 14 CFR Part 91, and had departed less than one minute before. The FAA reported that the accident flight was the second glider flight that day for the pilot, who had flown about 20 minutes on an earlier flight. Several witnesses observed the glider which was under tow, and then pitched up, down, and then up in excess of 45 degrees, at which time the tow rope broke. The glider then entered a right turn, and then entered a right spin of about 1 1/2 turns prior to impacting the ground, next to parked airplanes. The pilot was taken to a local hospital where he succumbed to his injuries on the following day. The pilot did not possess a FAA Airman Medical Certificate, nor was he required to possess one. The glider was examined by an FAA Airworthiness Inspector who reported, "...The tail flight control surfaces have continuity between the flight control attachments and the linkage/bellcrank, under the pilot's floor boards...." According to the Medical Examiner's Office, State of Massachusetts, a post-mortem examination of pilot did not disclose evidence of an incapacitating medical condition. Several witnesses observed the glider as it was being towed during takeoff. They reported that after becoming airborne, it pitched up, down, and up again, in excess of 45 degrees, then the tow rope broke. The glider then entered a right turn and rolled into a 1-1/2 turn spin to the right. Subsequenlty, the glider impacted in a grassy area next to parked airplanes on the airport. The pilot was taken to a local hospital, where he succumbed to his injuries the following day. No evidence of a preimpact mechanical failure or malfunction was found, and flight control continuity was confirmed. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_NYC96LA140.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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