NTSB CAROL · Event
Event NYC94LA140
Registry · N2282Z
FAA Aircraft Registry record.
Make / Model
CAPONE-ROCCO CUBY MODEL-B
Engine
CONT MOTOR A&C65 SERIES (65 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19781108
ADS-B equipped
Yes — Mode-S A2016F
Registrant of record
VOLVSKI JOEL T
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A LOSS OF ENGINE POWER FOR UNDETERMINED REASONS.
Factual narrative
On July 24, 1994, at 0945 eastern daylight time, a homebuilt Cuby B, N2282Z, owned and piloted by Joseph Marsilio, was substantially damaged when it collided with trees during a forced landing after takeoff from the Waterbury Airport, Waterbury, Connecticut. The pilot received serious injuries. Visual meteorological conditions prevailed and no flight plan had been filed for the flight operating under 14 CFR 91. In the NTSB Form 6120.1/2, the pilot stated that he had departed the southwest runway and was climbing out when the engine lost power. The pilot attempted to make a 180 degree turn back to the airport. According the Federal Aviation Administration (FAA) Inspector, the pilot stated to him that the engine failed shortly after lifting off runway 18. While the pilot was attempting to make the 180 degree turn, the airplane struck trees southeast of runway 36. The FAA Inspector conducted a post accident examination of the airplane. In his report he stated, "...The inspection was unable to find any visual sign of a mechanical defect that would have cause the engine to cease operation. The temperature and dew point conditions at the time of the accident were reviewed. According to the FAA-P-8740-24 Chart, Tips on Winter Flying, the conditions were conducive for moderate icing during cruise power, or serious icing in a powered glide. DURING THE INITIAL CLIMB AFTER TAKEOFF, THE ENGINE OF THE HOMEBUILT AIRPLANE EXPERIENCED A COMPLETE LOSS OF POWER. THE PILOT ATTEMPTED A 180 DEGREE TURN BACK TO THE AIRPORT, BUT THE AIRPLANE COLLIDED WITH TREES SHORT OF THE RUNWAY. EXAMINATION OF THE ENGINE REVEALED NO DISCREPANCIES. ACCORDING TO A CHART PUBLISHED BY THE FAA, THE TEMPERATURE AND DEW POINT WERE CONDUCIVE FOR MODERATE ICING DURING CRUISE POWER AND SERIOUS ICING DURING A POWERED GLIDE. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1994_NYC94LA140.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 ↗