NTSB CAROL · Event
Event NYC01LA182
Registry · N17AV
FAA Aircraft Registry record.
Make / Model
PIPER PA-28-181
Year of manufacture
1983 · 18 years old at event
Engine
LYCOMING O&VO-360 SER (180 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19830516
ADS-B equipped
Yes — Mode-S A116E8
Registrant of record
WESTCHESTER FLYING CLUB INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to attain a proper touchdown point. A factor was the tailwind.
Factual narrative
On July 21, 2001, about 1415 eastern daylight time, a Piper PA-28-181, N17AV, was substantially damaged during an overrun at Mattituck Airbase (21N), Mattituck, New York. The certificated private pilot and three passengers were not injured. Visual meteorological conditions prevailed at the time of the accident. No flight plan had been filed for the flight, between Igor I. Sikorsky Memorial Airport (BDR), Bridgeport, Connecticut, and Mattituck. The personal flight was conducted under 14 CFR Part 91. According to the pilot, while approaching the airport, he observed a Mooney on a 4-mile final to runway 01. He followed the Mooney, but when he was on final, saw that it had not yet cleared the runway, and executed a go-around. At the time, the windsock indicated that the winds were from the west-northwest. The pilot completed the next approach, and the airplane touched down, with full flaps, 200-300 feet from the runway threshold. The pilot felt that the touchdown speed was faster than he was accustomed to, but felt an aborted landing would have been too dangerous, since there were trees at the end of the runway. The pilot attempted to stop the airplane on the runway; however, the braking was limited. The airplane approached the departure end of the runway at an estimated 10-15 mph. It then rolled off the end of the runway and struck trees. The pilot felt that during the approach, the wind had shifted to a "significant" tailwind. According to a Federal Aviation Administration (FAA) inspector, witnesses reported that the airplane landed about halfway down the runway at a high rate of speed. The FAA inspector also noted that wind indications could be different at each end of the runway. Runway 01 was 2,200 feet in length, and 130 feet in width, with trees at the northern end. According to the PA-28-181 Pilot's Operating Handbook, the landing roll at sea level pressure, 25 degrees Centigrade, a gross weight of 2,500 pounds, full flaps, full-stall touchdown, and a zero-wind condition should have been approximately 950 feet. A 5-knot tailwind (the maximum for which data was provided) should have required about 1,280 feet. Winds, recorded at an airport about 10 nautical miles to the southwest at the approximate time of the accident, were from 200 degrees true, at 9 knots. The temperature was 24 degrees Centigrade. The pilot followed another airplane into the airport, and landed about halfway down the 2,200-foot runway at a high rate of speed. The airplane then departed the end of the runway at 10-15 mph. The pilot stated that the windsock indicated winds varying from approximately 35-80 degrees off the runway heading, but that during the approach, the wind shifted to a tailwind. Recorded winds at an airport 10 nautical miles away also indicated a tailwind. According to the Pilot's Operating Handbook, at 2,500 pounds, with a full-stall touchdown and full flaps in a zero wind, the airplane should have required about 950 feet of runway. With a 5-knot tailwind, it should have required about 1,280 feet of runway. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_NYC01LA182.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, go-around). 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 …
- NASA NTRS 2025 · Conference Paper
A Training Study to Improve Monitoring During A Go-Around
As part of an FAA program to improve go-around (GA) safety, we were asked to determine if we could improve the performance of the Pilot Monitoring (PM) during a GA maneuver.
- Flight Safety Foundation 2024 · FSF / AeroSafety World
Go-Around Safety Forum Findings
Foundation Go-Around Safety Forum technical findings — examines why pilots fail to execute go-arounds when criteria are met (stabilized approach gate not met, energy state out of envelope, traffic con…
- 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…
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