NTSB CAROL · Event
Event NYC96LA016
Registry · N65852
FAA Aircraft Registry record.
Make / Model
SCHWEIZER SGS 2-33A
Engine
NONE NONE
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19740621
ADS-B equipped
Yes — Mode-S A8AD94
Registrant of record
PETERSON ADAM
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper inflight planning/decision, which resulted in his failure to return to the airport after encountering an area of no thermal lift, and his failure to maintain adequate airspeed, while maneuvering to avoid an obstruction during an off airport landing.
Factual narrative
On October 22, 1995, about 1430 eastern daylight time, a Schweizer SGS 2-33 glider, N65852, was substantially damaged when it struck the ground in Barre, Massachusetts. The private pilot received minor injuries. Visual meteorological conditions prevailed, and no flight plan had been filed for the local flight which had departed the Tanner-Hiller Airport, Barre, at 1400, and was operated under 14 CFR Part 91. In the NTSB Accident Report, the pilot stated: Takeoff & tow to 3000 ft AGL normal Thermaled to 3350 Experienced heavy sink - Tried to return to airport Flew into a position where I wouldn't continue because of utility pole Turned left - left wing contacted ground - aircraft rotated 180 degrees When interviewed, the pilot reported that the glider stalled during the turn, at an altitude of about 25 feet above the ground. According to the FAA, the left wing was bent outboard of the strut attach point, and the fuselage was bent about 6 feet behind the cockpit. THE GLIDER PILOT REPORTED THAT WHILE THERMAL SOARING AT AN ALTITUDE OF 3350 FEET, HE ENCOUNTERED SINKING AIR. HE STATED THAT HE TRIED TO RETURN TO THE DEPARTURE AIRPORT, BUT SUBSEQUENTLY HEADED FOR AN OPEN FIELD ONE-HALF MILE FROM THE AIRPORT. HOWEVER, A UTILITY POLE WAS IN HIS PATH. DURING A TURN TO AVOID THE POLE, THE GLIDER WAS REPORTED TO HAVE STALLED ABOUT 25 FEET ABOVE THE GROUND AND STRUCK THE GROUND IN A NOSE DOWN, LEFT WING LOW ATTITUDE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_NYC96LA016.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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