NTSB CAROL · Event
Event NYC01LA019
Aircraft involved
Probable cause & findings
An improperly planned approach which resulted in an inadvertent stall.
Factual narrative
On October 23, 2000, at 0912 Eastern Daylight Time, an American AA-1A, N9375L was substantially damaged while landing at Westchester County Airport (HPN), White Plains, New York. The certificated commercial pilot and passenger received serious injuries. Visual meteorological conditions prevailed for the personal flight, that originated at Barnes Municipal Airport (BAF), Westfield, Massachusetts. No flight plan had been filed for the flight, which was conducted under 14 CFR Part 91. In the NTSB Form 6120.1/2 Pilot/Operator Aircraft Accident Report, the pilot stated: "I was # 2 to the airport on a right base for Runway 29. The # 1 A/C was on final to Runway 34. Upon turning right base to final for Runway 29, I noticed I was being blown to the left of the Runway 29 centerline. I attempted to get back on centerline with additional bank, but remember saying to myself not to bank too steeply. At that point the A/C suddenly apparently went into an accelerated stall at about 200 ft AGL. The A/C seemed to impact the runway in a wallowing mushy attitude. Loss of control seemed very sudden...." According to an inspector from the Federal Aviation Administration (FAA), a witness observed the airplane in a steep right bank, turn final, then descend toward the runway. The airplane was observed to strike the runway in a right wing low attitude, bounce, and then depart the runway on the right side. After the airplane came to rest, a fire developed under the fuselage. Several people grabbed fire extinguishers and proceeded to the scene. The occupants were assisted in exiting the airplane, and the airport fire-fighting personnel extinguished the fire. The FAA inspector further reported the initial touchdown occurred on runway centerline, in the middle of the displaced threshold for Runway 29. The airplane came to rest prior to crossing taxiway ALPHA, and the start of the landing area. He also reported that the landing gear had collapsed rearward, and the propeller was bent. Wrinkles were observed on both wings, the fuselage, and firewall. Gouge marks were also visible in the displaced threshold surface. The winds were from 060 degrees at 5 knots. The pilot reported that he was on a right base leg to Runway 29, when the airplane overshot the turn to final. He further reported that he increased the bank to return to runway centerline. The airplane suddenly entered an accelerated stall about 200 feet above the ground, and struck the runway. The FAA inspector reported the airplane touched down on centerline of Runway 29, in the middle of the displaced threshold. It then departed the right side of the runway and came to rest. A small fire developed under the fuselage, which was extinguished. The winds were from 060 degrees at 5 knots. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_NYC01LA019.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, loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Semantic Scholar 2016 · Article (Interacción)
Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report
Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- 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)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- arXiv 2025 · arXiv preprint
Quadratic Programming Approach to Flight Envelope Protection Using Control Barrier Functions
Ensuring the safe operation of aerospace systems within their prescribed flight envelope is a fundamental requirement for modern flight control systems.
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
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