NYC03LA003
2002-10-01 · Edgartown, Massachusetts, United States · None · 1 aircraft · Status: Completed
Airport 1B2
Current FAA registration · N8071Z
- Make / Model
- PIPER PA-28-181
- Year of manufacture
- 1981 · 21 years old at event
- Engine
- LYCOMING O&VO-360 SER (180 hp)
- Seats / Engines
- 4 seats · 1 engine
- Last airworthiness date
- 19811222
- ADS-B equipped
- Yes — Mode-S AAFE71
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadequate in-flight evaluation of the landing facilities wind conditions, and inadequate airspeed resulting in a stall/mush. A factor related to the accident was the tailwind condition.
Factual narrative
On October 1, 2002, about 1050 eastern daylight time, a Piper PA-28-181, N8071Z, was substantially damaged during a go-around from the Katama Airport, Edgartown, Massachusetts. The certificated commercial pilot and passenger were not injured. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight conducted under 14 CFR Part 91. According to the pilot, upon arriving in the airport area, he determined that the wind was favoring runway 06; a 2,700-foot long, 50-foot wide, turf runway. While on approach to runway 06, severe turbulence and a wind shift was encountered. After crossing the threshold of the runway, the airplane appeared to be landing with a tailwind, and the pilot initiated a go-around. During the go-around, as the pilot pulled back on the control yoke, the airplane continued to descend toward the ground. The airplane struck a tree, touched down in a grass field located beyond the departure end of the runway, and came to rest upright. The pilot additionally reported he did not experience any difficulties with the engine or airframe during the flight. Examination of the wreckage by a Federal Aviation Administration inspector revealed substantial damage to the lower empennage section of the airplane. The examination did not reveal any mechanical anomalies with the engine or airframe. The recorded weather at a nearby airport, at 1053, included winds from 250 degrees at 16 knots, gusting to 21 knots. The recorded winds at 0953 were from 260 degrees at 12 knots, gusting to 19 knots. Arriving in the airport area, the pilot determined that the wind was favoring runway 06. While on approach to runway 06, severe turbulence and a wind shift was encountered. After crossing the threshold of the runway, the airplane appeared to be landing with a tailwind, and the pilot initiated a go-around. During the go-around, as the pilot pulled back on the control yoke, the airplane continued to descend towards the ground. The airplane struck a tree, touched down in a grass field located beyond the departure end of the runway, and came to rest upright. The recorded weather at a nearby airport, about the time of the accident, included winds from 250 degrees at 16 knots, gusting to 21 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_NYC03LA003.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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Related research
Matched on aircraft type or causal vocabulary (stall, go-around, turbulence). All research papers
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- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA) Comparative Study on the Prediction of Aerodynamic Characteristics of Mini - Unmanned Aerial Vehicle with Turbulence Models
When dealing with CFD simulations the turbulent nature is seen on most of the engineering flows and these flows need to be solved.
- arXiv 2020 · arXiv preprint Numerical Simulation of Iced Wing Using Separating Shear Layer Fixed Turbulence Models
Aerodynamic prediction of glaze ice accretion on airfoils and wing is studied using the Reynolds-averaged Navier-Stokes method.
- NASA NTRS 2019 · Conference Paper Prediction of stall and post-stall behavior of airfoils at low and high Reynolds numbers
An interactive boundary-layer method, together with the e(super n)-approach to the calculation of transition, has been used to predict the stall and post-stall behavior of airfoils at low and high Rey…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA) Low Level Turbulence Detection For Airports
Abstract—— Low level wind shear and turbulence present a serious safety risk to aircraft during the approach, landing and take-off phases.
- Embry-Riddle Scholarly Commons 2018 · Journal article (IJAAA) Evaluating the Effect of Turbulence on Aircraft During Landing and Take-Off Phases
—— Low level wind shear and turbulence present a serious safety risk to aircraft during the approach, landing and take-off phases.