NTSB CAROL · Event
Event NYC95LA131
Registry · N43705
FAA Aircraft Registry record.
Make / Model
TAYLORCRAFT BC12-D
Year of manufacture
1946 · 49 years old at event
Engine
CONT MOTOR A&C65 SERIES (65 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19561010
ADS-B equipped
Yes — Mode-S A53F95
Registrant of record
KELLER WILLIAM R
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadequate preflight inspection, which failed to detect water-contaminated fuel which resulted in the loss of engine power. Also causal was the pilot's failure to maintain airspeed during the forced landing, which resulted in the inadvertent stall/spin and collision with the terrain.
Factual narrative
On June 1, 1995, at 1430 eastern daylight time, a Taylorcraft BC-12, N43705, was substantially damaged during a forced landing after takeoff from the Geneseo Airport, Geneseo, New York. The private pilot was seriously injured and the passenger received minor injuries. Visual meteorological conditions prevailed, for the personal flight originating at Geneseo. No flight plan had been filed for the flight conducted under 14 CFR Part 91. The pilot and passenger flew from Lancaster, New York, to the Geneseo Airport (D52), the day of the accident. While at D52, the pilot purchased auto fuel from a local vendor to refuel his airplane, and used plastic containers to transport the fuel. After about 45 minutes of ground time at D52, the pilot and passenger boarded the airplane for the return trip to Lancaster. In the NTSB Form 6120.1/2, the pilot stated that he performed a soft field takeoff at D52, and during the initial climb the engine lost power. He then observed trees and power lines at the end of the runway, and elected to attempt a landing to the left of the runway. The pilot further stated: ...Airplane proceeded to glide normally, then at approximately 100 feet, the nose of the aircraft dropped straight down and the aircraft plunged to the ground... In a written statement, a witness to the accident said: ...I heard an aircraft engine miss. I looked north towards the runway and saw a blue and white aircraft at about 100 feet. It's engine quit, and it turned and dived vertically to the left, hitting the ground. A Federal Aviation Administration Airworthiness Inspector examined the wreckage at the accident site. The Inspector's report stated that the airplane's three fuel tanks contained auto fuel, and the carburetor bowl contained water and sediment. The Inspector also examined the plastic containers used to transport the auto fuel to the airplane. His report stated, "...it appears the same sediments and water drained from the carburetor bowl were found in the plastic containers..." THE AIRPLANE LANDED AT A LOCAL AIRPORT, WHERE THE PILOT PURCHASED AUTO FUEL FROM A VENDOR. PLASTIC CONTAINERS WERE USED TO TRANSPORT THE FUEL TO THE AIRPLANE. DURING INITIAL CLIMB AFTER TAKEOFF, THE ENGINE LOST POWER AND THE PILOT MADE A FORCED LANDING. DURING THE LANDING THE AIRPLANE NOSED OVER. EXAMINATION REVEALED THE AIRPLANE'S FUEL TANKS ALL CONTAINED AUTO FUEL, AND THE CARBURETOR BOWL CONTAINED WATER AND SEDIMENT. THE PLASTIC CONTAINERS USED TO TRANSPORT THE FUEL ALSO CONTAINED WATER AND SEDIMENT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_NYC95LA131.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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