NTSB CAROL · Event
Event NYC00LA254
Registry · N8704P
FAA Aircraft Registry record.
Make / Model
PIPER PA-24-260
Year of manufacture
1965 · 35 years old at event
Engine
LYCOMING TI0-540 SER (310 hp)
Seats / Engines
4 seats · 1 engine
Last airworthiness date
19650312
ADS-B equipped
Yes — Mode-S ABF948
Registrant of record
LARSON ALYSIA E
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to attain the proper touchdown point.
Factual narrative
On September 7, 2000, about 1800 Eastern Daylight Time, a Piper PA-24-260, N8704P, was substantially damaged during a landing at Seamans Field (9N3), Factoryville, Pennsylvania. The certificated commercial pilot was not injured, and visual meteorological conditions prevailed at the time of the accident. No flight plan had been filed for the personal flight, conducted under 14 CFR Part 91. According to a Federal Aviation Administration (FAA) inspector, the pilot reported that he was practicing a short field landing, and "must have gotten behind the airplane." The airplane touched down about 1 foot short of the runway, broke the left landing gear, bent the right landing gear, and damaged both wings. The pilot also noted that there were no mechanical problems with the airplane. The pilot stated that he had returned from a day trip, and made a full-stop landing at dusk. He then taxied back, took off, and flew a pattern for a practice short field landing to Runway 22. During the landing, the airplane struck a runway threshold light, the left landing gear strut collapsed, and the airplane veered off to the left. The pilot also reported that he had over 9,400 hours of flight time. Winds, recorded at an airport 12 nautical miles to the south, about 1/2 hour before the accident, were from 180 degrees true, at 8 knots. During a practice short field landing at dusk, the airplane touched down about 1 foot short of the runway. It struck a runway threshold light, the left landing gear strut collapsed, and the airplane veered off to the left. There were no mechanical problems with the airplane, and the commercial pilot had over 9,400 hours of flight time. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2000_NYC00LA254.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 (icing). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Mathematical Model on the Temporal Dynamics of Aviation Competitive Pricing
This study investigates the competitive dynamics of airport pricing using U.S. airport data to validate the findings. It employs linear and nonlinear ordinary differential equation models to analyze t…
- NASA NTRS 2025 · Presentation
NASA Icing Update – March 2025
This NASA Icing Update was prepared for presentation to the SAE International AC-9C Inflight Icing Technology Committee. This update includes the following topics: planned Rotational Icing Scaling tes…
- arXiv 2024 · arXiv preprint
An energy-stable phase-field model for droplet icing simulations
A phase-field model for three-phase flows is established by combining the Navier-Stokes (NS) and the energy equations, with the Allen-Cahn (AC) and Cahn-Hilliard (CH) equations and is demonstrated ana…
- NASA NTRS 2024 · Presentation
NASA Icing Update – Oct 2024
This presentation provides a status update on select NASA icing research activities for the SAE AC-9C Icing Technical Committee Meeting on Oct 21, 2024.
Browse the full corpus — academia portal ↗