ERA10CA473
2010-09-09 · Montauk, New York, United States · None · 1 aircraft · Status: Completed
Airport MTP
Aircraft involved
Probable cause & findings
The pilot's inadequate compensation for crosswind conditions which resulted in a hard landing and loss of directional control.
Factual narrative
According to the pilot, as he approached his destination airport, he radioed the Unicom and requested airport advisories. He was advised that traffic was landing on runway 24, and the wind was reported at 310 degrees at 9 knots. During his first approach he believed he was too high and executed a go-around. He re-entered the pattern from the northwest for landing. As he descended down to the "numbers" a wind shear struck the airplane and the stall alarm sounded along with a drop in airspeed. He made an attempt to go-around, but was to "low and slow". He was unable maintain altitude, landed hard and veered off of the left side of the runway. The airplane struck some small trees and the right wing was torn from the fuselage. The reported wind at the accident airport near the accident time was from 290 degrees at 10 knots, gusting to 18 knots. According to the pilot, as he approached his destination airport, he requested airport advisories over the UNICOM frequency. He was advised that traffic was landing on runway 24, and the wind was reported at 310 degrees at 9 knots. During his first approach he believed he was too high and executed a go-around. He re-entered the pattern and as the airplane descended to the runway, it encountered windshear and stalled. The pilot made an attempt to go-around, but the airplane was too low and slow. He was unable to maintain the airplane's altitude, and it landed hard and veered off the left side of the runway. The airplane struck trees and the right wing was torn from the fuselage. The reported wind at the accident airport near the accident time was from 290 degrees at 10 knots, gusting to 18 knots. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- C Personnel issues-Action/decision-Action-Incorrect action performance-Pilot - C
- C Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Response/compensation - C
Verbatim from NTSB's published report. Source file
NTSB_2010_ERA10CA473.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (wind shear, stall, go-around). All research papers
- NASA NTRS 2019 · Conference Paper Optimal recovery from microburst wind shear
The flight path of a twin-jet transport aircraft is optimized in a microburst encounter during approach to landing. The objective is to execute an escape maneuver that maintains safe ground clearance …
- NASA NTRS 2013 · Conference Paper Optimal nonlinear estimation for aircraft flight control in wind shear
The most recent results in an ongoing research effort at Princeton in the area of flight dynamics in wind shear are described.
- 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.