NTSB CAROL · Event
Event NYC95LA166
Registry · N11JK
FAA Aircraft Registry record.
Make / Model
TIMOTHY HOWEN PITTS S-1C
Year of manufacture
2024
Engine
LYCOMING 0-290 SERIES (140 hp)
Seats / Engines
1 seats · 1 engine
Last airworthiness date
20250916
ADS-B equipped
Yes — Mode-S A02AAC
Registrant of record
HOWEN TIMOTHY RAY
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's premature liftoff which resulted in an inadvertent stall and a subsequent collision with trees.
Factual narrative
On July 18, 1995, at 2030 eastern daylight time, a Beech V35B, N11JK, sustained substantial damage when it collided with a tree during the takeoff from a private airport in Goshen, Ohio. The commercial pilot and one passenger were not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the flight conducted under 14 CFR Part 91. The pilot initiated the takeoff on runway 06, which was a grass runway, 1640 feet long. In a statement taken by the Ohio state highway patrol, the pilot stated: ...We had landed and were starting to leave and started to taxi. We were at the very end of the field, and I gave it full throttle and started down the runway. We lifted off and then came back down and then lifted off again....[The airplane] started to veer to the left, so I gave it right rudder and that's when I clipped the trees and came to rest on the other side of the tree line.... The pilot rated passenger stated: ...When we had approximately 50 knots, I encouraged the pilot to lift the nosewheel clear of the ground. He did this. It dropped back immediately making contact with the ground, once more bouncing clear. The plane skipped into the air, the nose dropped again, a bit quicker. It bounced up again as the pilot applied back pressure and we were airborne. The stall warning horn began blaring....We made ground contact, and once again the nose bounced upward with an apparent addition of back pressure by the pilot. We were airborne in a nose high attitude with about 500 to 600 feet of runway remaining...the left wing dropped....[The pilot]...applied full right rudder. The wing lifted, the nose remained high....The left wing made contact with...shrubs...to the left...of the runway.... The FAA Inspector reported, "The pilot...stated...that the aircraft failed to reach flying speed and that he tried to pull the aircraft off the ground prior to reaching the end of the runway." Additionally, the pilot reported that there were no mechanical malfunctions with the airframe or engine, and that the winds were calm at the time of the accident. THE PILOT PERFORMED THE TAKEOFF ON RUNWAY 06, A GRASS RUNWAY, 1640 FEET LONG. DURING THE TAKEOFF THE AIRPLANE SETTLED BACK TO THE RUNWAY AND BOUNCED SEVERAL TIMES. THE PILOT RATED PASSENGER STATED, '[DURING THE TAKEOFF], I ENCOURAGED THE PILOT TO LIFT THE NOSEWHEEL CLEAR OF THE GROUND....IT DROPPED BACK IMMEDIATELY....IT BOUNCED UP AGAIN AS THE PILOT APPLIED BACK PRESSURE....THE STALL WARNING HORN BEGAN BLARING....AS WE CLIMBED NOSE HIGH, THE LEFT WING DROPPED (STALL)....THE LEFT WING MADE CONTACT WITH TOP OF THE SHRUBS....' THE FAA INSPECTOR REPORTED, 'THE PILOT...STATED...THAT THE AIRCRAFT FAILED TO REACH FLYING SPEED AND THAT HE TRIED TO PULL THE AIRCRAFT OFF THE GROUND PRIOR TO REACHING THE END OF THE RUNWAY.' THE PILOT REPORTED THAT THERE WERE NO MECHANICAL MALFUNCTIONS WITH THE AIRPLANE, AND THAT THE WINDS WERE CALM AT THE TIME OF THE ACCIDENT. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_NYC95LA166.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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