CEN14LA144
2014-02-13 · Galion, Ohio, United States · None · 1 aircraft · Status: Completed
Airport GQQ
Current FAA registration · N3882J
- Make / Model
- CESSNA 150G
- Year of manufacture
- 1966 · 48 years old at event
- Engine
- CONT MOTOR 0-200 SERIES (100 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19660927
- ADS-B equipped
- Yes — Mode-S A47BA9
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
A total loss of engine power on climbout for reasons that could not be determined because postaccident examination of the engine did not reveal any anomalies that would have precluded normal operation.
Factual narrative
On February 19, 2014, about 1130 eastern standard time (EST), a Cessna 150G airplane, N3882J, made a forced landing following a total loss of engine power after takeoff from the Galion Municipal Airport (GQQ), Galion, Ohio. The certificated private pilot and passenger were not injured. The airplane sustained substantial damage. The airplane was registered to and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed for the flight and no flight plan was filed. The flight was originating at the time of the accident. In a statement provided to the National Transportation Safety Board (NTSB) investigator-in-charge (IIC), the pilot reported no abnormalities or fuel contaminates were observed during the preflight airplane inspection. After engine start-up, the pilot allowed the airplane engine temperature to rise before taxiing due to the cold ambient temperature. The pre-departure run-up was normal and he noted the takeoff was smooth until about 400-500 feet above ground level when the engine "misfired." The pilot stated he pulled the carburetor heat, checked the primer was in the "locked" position and verified the fuel selector valve was in the "on" position. The engine then experienced a total loss of power. Unable to restore engine power, he made a forced landing into an agricultural field. During the forced landing the airplane sustained substantial damage to the fuselage and engine mounts. The airplane was a two seat, high wing, tricycle landing gear, airplane which was manufactured in 1967. It was powered by a Continental Motors O-200 engine. An FAA inspector conducted a postaccident examination of the airplane engine and fuel system. The examination revealed engine continuity of the crankshaft, lifters and valves. Compression was present in all four cylinders. There were also sparks observed in all 8 ignition wires. Fuel samples were taken from the fuel lines, carburetor, and gascolator with no visible signs of water. The airframe fuel sump was drained and a "few drops" of water were observed. At the direction of the NTSB IIC, the carburetor was opened and no anomalies were observed with the carburetor float. In addition, the fuel was tested with water indicating paste to detect water contamination. The water indicating paste did not reflect water contaminates in the fuel. The closest weather reporting facility was the Mansfield Lahm Regional Airport, Mansfield, Ohio. At 1052, an aviation routine weather report (METAR) from the Mansfield Lahm Regional Airport, 12 miles northeast of the accident site, reported wind from 030 degrees at 5 knots; sky condition, clear; visibility, 9 statute miles; temperature 21 degrees F; dewpoint 7 degrees F; barometric pressure 29.84 inches of mercury. According to a carburetor icing probability chart, an airplane operating in the ambient conditions near the accident site could expect no carburetor icing while at cruise or glide power. The pilot reported that he found no abnormalities with the airplane during the preflight inspection. After engine start-up and before taxiing, the pilot allowed the engine temperature to rise due to the cold ambient temperature, and the predeparture engine run-up was normal. The airplane took off and, when it reached about 500 ft above ground level, the engine "misfired." The pilot cycled the carburetor heat on and verified that the primer was "locked" and that the fuel selector was in the "on" position. Despite these actions, the engine experienced a total loss of power. The pilot subsequently conducted a forced landing in an agricultural field. A postaccident examination of the engine revealed no evidence of any preimpact mechanical malfunctions or fuel contamination that would have precluded normal operation. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- — Environmental issues-Physical environment-Terrain-Sloped/uneven-Contributed to outcome
- C Not determined-Not determined-(general)-(general)-Unknown/Not determined - C
Verbatim from NTSB's published report. Source file
NTSB_2014_CEN14LA144.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (icing, fuel contamination). All research papers
- arXiv 2026 · arXiv preprint Enabling Beyond-Visual-Line-of-Sight Drones Operation over Open RAN 5G Networks with Slicing
Among the foretold claims of the transition from 5G to 6G, Beyond-Visual-Line-of-Sight (BVLoS) drone operation has emerged as a prominent Internet-of-Robots enabler.
- 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…
- 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…
- 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…
- 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…