NTSB CAROL · Event
Event ATL97LA015
Aircraft involved
Probable cause & findings
The loss of engine power for undetermined reasons.
Factual narrative
On November 1, 1996, at 1745 eastern standard time, a Piper PA-28-161, N81435, collided with two travel trailers in a secure lot east of the Hernando County Airport in Brooksville, Florida. The instructional flight operated under the provisions of Title 14 CFR Part 91 with no flight plan filed. Visual weather conditions prevailed at the time of the accident. The airplane sustained substantial damage, and the student pilot was not injured. The flight departed Brooksville, at 1730. The aircraft owner reported that the student pilot was conducting traffic pattern training when he experienced a total loss of engine power while on final approach to runway 27. The student pilot reported that he completed the before landing check, that included the application of carburetor heat. After the student pilot turned on to the final approach leg, he noticed that the engine had quit. The student pilot selected an area near the airport and attempted a forced landing. During the forced landing roll out, the airplane collided with two parked vehicles. The examination of the aircraft at the accident site failed to disclose a mechanical problem. A subsequent functional check of the engine disclosed that it operated normally throughout all power ranges. This check was repeated with the same results. A review of the weather data disclosed that conditions were favorable for the formation of carburetor icing. The aircraft owner reported that the student pilot was conducting traffic pattern training when he experienced a total loss of engine power while on final approach. The student pilot reported that he completed the before landing check that included the application of carburetor heat. After he turned on to the final approach leg the student pilot noticed that the engine had quit. During the forced landing roll the airplane collided with two parked vehicles. The examination of the aircraft at the accident site failed to disclose a mechanical problem. A subsequent functional check of the engine disclosed that it operated normally throughout all power ranges. Weather conditions were favorable for the formation of carburetor ice. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_ATL97LA015.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 ↗