NTSB CAROL · Event
Event NYC07LA192
Aircraft involved
Probable cause & findings
A partial loss of engine power for undetermined reasons.
Factual narrative
On August 12, 2007, about 1830 eastern daylight time, a Piper J-3, N6429H, was substantially damaged during a forced landing in Frenchtown, New Jersey. The certificated private pilot and the passenger incurred minor injuries. Visual meteorological conditions prevailed, and no flight plan had been filed for the local flight from Vansant Airport (9N1), Erwinna, Pennsylvania. The personal flight was conducted under 14 Code of Federal Regulations Part 91. According to the pilot, he took off about 1815, and climbed the airplane to 1,400 feet above mean sea level. He then turned left over the Delaware River, applied carburetor heat to the Continental C85-12 engine, and descended to approximately 500 feet above the water. He then secured the carburetor heat and opened the throttle, but there was no engine response. The engine "sounded o.k." but remained at idle power regardless of throttle position. The pilot checked that the fuel selector was on, and 300 to 400 feet above the river, turned toward the shoreline. He attempted a forced landing to a field; however, prior to reaching it, the airplane descended into a tree. There was no on-scene examination of the airplane. It was removed from the tree, transported to a storage facility in Delaware, and subsequently sold for salvage. While in the storage facility, the owners performed a cursory examination, with no preaccident mechanical anomalies noted. Weather, reported at an airport 12 nautical miles to the east, at 1854, included winds from 260 degrees true at 6 knots, visibility 10 miles, a broken cloud layer at 7,000 feet, temperature 30 degrees Celsius (C), dew point 13 degrees C, and an altimeter setting of 29.96 inches Hg. Plotting the temperature and dew point values on a carburetor icing chart yielded a probability of serious carburetor icing at glide power. The pilot climbed the airplane to 1,400 feet above mean sea level. He turned left over a river, applied carburetor heat to the engine, and descended the airplane to approximately 500 feet above the water. He then secured the carburetor heat and opened the throttle, but there was no engine response. The engine "sounded o.k." but remained at idle power regardless of throttle position. The pilot checked that the fuel selector was on, and 300 to 400 feet above the river, turned the airplane toward a shoreline. The pilot attempted a forced landing to a field; however, prior to reaching it, the airplane descended into a tree. No examination of the airplane was performed at the accident scene, and a cursory examination by the owner at a later date yielded no preaccident mechanical anomalies. Ambient temperature and dew point values indicated a probability of serious carburetor icing at glide power. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_NYC07LA192.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 ↗