NTSB CAROL · Event
Event NYC01LA188
Aircraft involved
Probable cause & findings
A loss of engine power for undetermined reasons.
Factual narrative
On July 25, 2001, about 1945 eastern daylight time, a Cessna 172P, N52266, was substantially damaged during a forced landing after takeoff from the Tipton Airport (FME), Odenton, Maryland. The certificated flight instructor (CFI) and student pilot were not injured. Visual meteorological conditions prevailed and no flight plan had been filed for the instructional flight conducted under 14 CFR Part 91. According to the CFI, the flight originated at the Freeway Airport (W00), Mitchellville, Maryland, about 1830. Prior to takeoff, during the engine run-up, the CFI experienced rough engine operation during the magneto check; however, after the mixture was leaned, he did not experience any further problems. After takeoff, the student pilot performed some ground reference maneuvers, and they then proceeded to Tipton to practice landings and takeoffs. They performed a full stop landing about 1935, and then completed the after landing and pre-takeoff checklists. During the subsequent takeoff from runway 28 at Tipton, when the airplane was about 200 feet above the ground, the engine experienced a partial loss of engine power. The application of carburetor heat did not have an effect on the engine's performance and the CFI was not able to maintain altitude. The CFI then performed a forced landing to a grassy area northwest of the runway; however, the airplane struck trees and a fence. Examination of the airplane and engine by a Federal Aviation Administration (FAA) inspector did not reveal any pre-impact failures. Fuel consistent with aviation gasoline was observed throughout the airplane's fuel system, and no evidence of contamination was noted. Additionally, the engine was started and ran uneventfully; however, due to damaged engine mounts, the rpm was not increased above 1,300. The temperature and dew point reported at an airport about 8 miles northeast of Tipton, at 1954, was 86 and 70 degrees F, respectively. A review of a FAA carburetor icing probability chart placed the reported temperature and dew point in the "serious icing at glide power" area of the chart. During takeoff, when the airplane was about 200 feet above the ground, the engine experienced a partial loss of engine power and the pilot was not able to maintain altitude. The pilot performed a forced landing to a grass area northwest of the runway; however the airplane struck trees and a fence. Examination of the airplane and engine did not reveal any pre-impact failures. Fuel consistent with aviation gasoline was observed throughout the airplane's fuel system, and no evidence of contamination was noted. Additionally, the engine was started and ran uneventfully; however, due to damaged engine mounts, the rpm was not increased above 1,300. The temperature and dew point reported at a nearby airport, was 86 and 70 degrees F, respectively. A review of a carburetor icing probability chart, placed the reported temperature and dew point in the "serious icing at glide power" area of the chart; however, the pilot reported that the application carburetor heat after the partial loss of engine power did not effect the engine's performance. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_NYC01LA188.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 ↗