NTSB CAROL · Event
Event NYC96LA093
Aircraft involved
Probable cause & findings
the pilot's improper flare and recovery from a bounced landing. A contributing factor was his lack of recent flight experience.
Factual narrative
On April 28, 1996, at 1030 eastern daylight time, a Cessna 172P, N98574, was substantially damaged during landing at the Rutland State Airport, Rutland, Vermont. The private pilot was not injured. Visual meteorological conditions prevailed for the personal flight that originated at Schenectady, New York, about 0930. A VFR flight plan had been filed for the flight conducted under 14 CFR Part 91. In the NTSB Form 6120.1/2, the pilot stated that he was landing at the Rutland State Airport (RUT) at the completion of a cross country flight. He stated that on final to runway 31, the airplane drifted to the left during the flare. He further stated: "...Attempted to reestablish alignment with runway and aircraft touched down and bounced. Aircraft touched down and veered sharply to the left and stopped in the sod near runway intersection...Wind sock indicated right quartering headwind from approximately 340 degrees..." In the Federal Aviation Administration (FAA) Inspector's report, he stated the pilot informed him that the wind gusts and turbulence caused the pilot to flare high. The airplane then stalled, hitting the runway on the nose wheel. The pilot did not attribute the accident to any mechanical malfunction. Winds reported by the Rutland AWOS at the time of the accident were from 300 degrees at 4 knots. The pilot's total flight experience was 99 hours, of which 36 hours were as a pilot-in-command. He had logged a total of 7 hours in this make and model, of which 5 hours were as pilot-in-command. The balance of his flight experience was in the Cessna 152. The pilot had flown 2 1/2 hours in the previous 90 days. The pilot had completed a cross country flight and was landing on runway 31. When the pilot flared, the airplane drifted to the left. During the pilot's attempt to realign the airplane with the runway, the airplane bounced and veered left off of the runway. Winds reported by the airport automatic weather observing/reporting system (AWOS) at the time of the accident were from 300 degrees at 4 knots. The pilot had logged 7 hours in this make and model, of which 5 hours were as pilot-in-command. The balance of his flight experience was in the Cessna 152. The pilot had flown 2-1/2 hours in the previous 90 days. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_NYC96LA093.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, turbulence). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- 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…
- arXiv 2026 · arXiv preprint
Direct Numerical Simulations of Ice-Ocean Boundary Turbulence
Turbulent heat and freshwater transport at ice-ocean interfaces controls glacier and iceberg melt rates, yet the underlying physics remains poorly constrained.
- 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 …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
Political Turbulence and Aviation Safety: A Cross-National Analysis of Political Stability's Effects on Aviation Accidents
To what extent does political stability affect aviation safety? This research aims to link domestic political conditions and public safety through the consideration of aviation accident frequency.
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