NTSB CAROL · Event
Event NYC07LA148
Registry · N14VS
FAA Aircraft Registry record.
Make / Model
HONDA AIRCRAFT CO LLC HA-420
Year of manufacture
2023
TCDS
A00018AT · HONDA AIRCRAFT COMPANY LLC
Engine
GE HONDA HF-120
Seats / Engines
8 seats · 2 engines
Last airworthiness date
20230811
ADS-B equipped
Yes — Mode-S A0A243
Registrant of record
VERUCA SALT LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's improper decision to attempt low altitude aerobatics, and his failure to maintain airspeed during the aerobatics, which resulted in an inadvertent stall while maneuvering.
Factual narrative
On June 24, 2007, about 1837 eastern daylight time, an amateur built Vans RV-4, N14VS, was substantially damaged while maneuvering near Wallkill, New York. The certificated commercial pilot and passenger were fatally injured. Visual meteorological conditions prevailed for the flight that departed Orange County Airport (MGJ), Montgomery, New York, about 1700. No flight plan was filed for the local personal flight conducted under 14 CFR Part 91. A witness was standing outside of his residence, and observed the accident airplane. The witness stated that the airplane was flying north, approximately 250 feet above ground level (agl). The airplane performed a barrel roll, and then entered a loop. The airplane had completed about half of the loop, when it "wobbled," dropped from the top of the loop, and dove straight into the ground. The witness added that the engine noise was continuous, with no changes noted. According to the airplane's logbook, it was manufactured from 1981 to 1983. The airplane's most recent annual condition inspection was completed on November 25, 2006. At that time, the airplane and the engine had accumulated 428.4 total hours of operation. According to Federal Aviation Administration (FAA) records, the pilot, age 70, held a commercial pilot certificate, with ratings for airplane single engine land and airplane multiengine land. The pilot's logbook was not recovered, and his aerobatic experience was unknown. His most recent FAA third class medical certificate was issued on November 22, 2005. At that time, the pilot reported a total flight experience of 1,000 hours. An autopsy was performed on the pilot at the Orange County Regional Medical Center, Middletown, New York. Toxicological testing was subsequently performed by the FAA Forensic Toxicology Research Team, Oklahoma City, Oklahoma. No preimpact medical anomalies were noted. The reported weather at MGJ, about 4 miles east of the accident site, at 1854, was: wind from 240 degrees at 6 knots; visibility 10 miles; sky clear; temperature 27 degrees Celsius (C); dew point 12 degrees C; altimeter setting 30.05 inches of mercury. The amateur-built experimental airplane was observed performing aerobatics about 250 feet above ground level. The airplane performed a barrel roll, then completed about half of a loop when it stalled at the top and descended straight into the ground. The engine ran continuously throughout the accident sequence, with no changes in power noted. The pilot had accumulated approximately 1,000 hours of total flight experience; however, no record of his aerobatic experience was recovered. The reported weather near the accident site, about the time of the accident, included clear skies, wind at 6 knots, and visibility 10 miles. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_NYC07LA148.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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