NTSB CAROL · Event
Event NYC95LA077
Aircraft involved
Probable cause & findings
The pilot's improper use of carburetor heat which resulted in carburetor icing and a subsequent loss of engine power. A factor is carburetor icing conditions.
Factual narrative
On, March 19, 1995 about 0915 eastern standard time, a Cessna 150J, N60949, operated by Lehigh Valley Aviation and piloted by Jon E. Goodman, was substantially damaged during an aborted takeoff at Slatington Airport, Slatington, Pennsylvania. The pilot and passenger were not injured. Visual meteorological conditions prevailed for the intended local flight conducted under 14 CFR Part 91. In the NTSB form 6120.1/2 the pilot reported, there was a light wind from the south and he departed runway 19. The pilot further stated: ...Normal build up of speed, became slightly hesitant around takeoff speed (60 MPH). 3/4 down the runway, engine RPM dropped, airspeed quickly dropped below 50 MPH. This is when I decided to abort. At most the airplane was 1 to 5 feet off the ground. In a telephone interview the pilot added, during the aborted takeoff the airplane porpoised on the runway. He reduced the power to idle, and applied brakes. The airplane overran the runway. The nose gear struck a log, and the airplane nosed over. According to the Airport Facility Directory, runway 19 is 2520 feet long with obstacles at both ends. The first 1950 feet is asphalt, and the remaining 570 is turf. According to the Federal Aviation Administration Inspector's statement, no malfunctions were detected in the engine or airframe. The statement further stated: ...The gascolator still had clean fuel in it and the fuel lines were still intact to the carburetor, which still had fuel....The air filter was [checked] for obstructions, and none were found....The top spark plugs were removed and all four cylinders [had] compression. The spark plugs [had] no deposits or fouling....The impulse coupling sounded normal when the propeller was rotated. The temperature and dew point at Allentown, Pennsylvania, 12 miles southeast of the accident scene were reported to be 44 degrees F and 36 degrees F respectively at 0845. Additionally, at 0945, the temperature and dew point were 48 degrees F and 34 degrees F. According to a carburetor icing probability chart, both sets of conditions were conducive for serious icing at cruise or climb power. THE PILOT REPORTED DURING THE TAKEOFF THERE WAS A LOSS OF ENGINE POWER. HE ELECTED TO ABORT THE TAKEOFF. DURING THE ABORTED TAKEOFF THE AIRPLANE PORPOISED AND OVERRAN THE RUNWAY. THE NOSE GEAR STRUCK A LOG AND THE AIRPLANE NOSED OVER. THE FEDERAL AVIATION ADMINISTRATION INSPECTOR'S POST ACCIDENT EXAMINATION REVEALED NO DISCREPANCIES WITH THE ENGINE OR AIRFRAME. THE TEMPERATURE AND DEW POINT AT ALLENTOWN, PENNSYLVANIA, 12 MILES SOUTHEAST WERE REPORTED TO BE 44 DEGREES F AND 36 DEGREES F RESPECTIVELY AT 0845. ADDITIONALLY, AT 0945, THE TEMPERATURE AND DEW POINT WERE 48 DEGREES F AND 34 DEGREES F. ACCORDING TO A CARBURETOR ICING PROBABILITY CHART, BOTH SETS OF CONDITIONS WERE CONDUCIVE FOR SERIOUS ICING AT CRUISE OR CLIMB POWER. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_NYC95LA077.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 ↗