ERA11CA331
2011-06-08 · Ghent, New York, United States · Serious · 1 aircraft · Status: Completed
Airport NY1
Aircraft involved
Probable cause & findings
The pilot's delayed decision to abort the landing and execute a go-around.
Factual narrative
According to the pilot, several minutes after takeoff the weather began to deteriorate and the sky turned black with convective activity reported in the area. He decided to divert to a nearby airport which had a 4,000-foot long by 75-foot wide turf runway. As the pilot approached the runway he could not determine where the approach end was located. The airplane approached the runway high and fast. The pilot did not think he would be able to stop the airplane before reaching the end of the runway, so he aborted the landing. One witness reported that the airplane aborted the landing with less than 1/4 of the runway's total length remaining. During the attempted climb out, the pilot felt that the engine felt less powerful and but could not recall any specific abnormal indications. Without sufficient airspeed to climb above approaching trees, the pilot stalled the airplane into a pond, resulting in substantial damage to the left wing and empennage. Examination of the airplane by a Federal Aviation Administration Inspector following the accident revealed no evidence of any pre-impact mechanical malfunctions or failures. The weather conditions reported at an airport 5 nautical miles southwest, about the time of the accident included a temperature of 35 degrees Celsius and a left quartering tailwind at 6 knots. According to the pilot, several minutes after takeoff the weather began to deteriorate and the sky turned black with convective activity reported in the area. He decided to divert to a nearby airport which had a 4,000-foot long by 75-foot wide turf runway. As the pilot approached the runway he could not determine where the approach end was located. The airplane approached the runway high and fast. The pilot did not think he would be able to stop the airplane before reaching the end of the runway, so he aborted the landing. One witness reported that the airplane aborted the landing with less than 1/4 of the runway's total length remaining. During the attempted climb out, the pilot thought that the engine felt less powerful but could not recall any specific abnormal indications. Without sufficient airspeed to climb above approaching trees, the pilot stalled the airplane into a pond, resulting in substantial damage to the left wing and empennage. A postaccident examination of the airplane revealed no evidence of any preimpact mechanical malfunctions or failures. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot - C
- C Personnel issues-Action/decision-Action-Delayed action-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2011_ERA11CA331.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 (stall, go-around). All research papers
- NASA NTRS 2023 · Reprint (Version printed in journal) Finite Element Simulation of Three Full-Scale Crash Tests for Cessna 172 Aircraft
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- NASA NTRS 2019 · Conference Paper Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM) Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- 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
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