NTSB CAROL · Event
Event ERA25LA216
Aircraft involved
Probable cause & findings
A total loss of engine power for reasons that could not be determined.
Factual narrative
The pilot and two passengers were on a multi-leg cross-country flight under instrument flight rules. After refueling the airplane fully, they departed on the accident flight and flew to an intermediate airport where the pilot performed a practice instrument approach. After landing the airplane and departing again, they flew toward the destination airport, where the pilot planned to perform another practice instrument approach. About 1-mile from the final approach fix, and while flying over the ocean, the airplane’s engine suddenly lost power. The pilot had his passenger inform air traffic control of the emergency before ditching the airplane into the water about 5 miles offshore. All three occupants incurred minor injuries and were rescued after the accident. The airplane was not recovered and presumed substantially damaged. Review of ADS-B data for the flight revealed that the airplane had been aloft for less than 2.5 hours since last being fueled to its full capacity of 38 gallons. According to the airplane’s Pilot Operating Handbook, at cruise power settings the airplane’s estimated consumption ranged from 8.0 to 9.0 gallons per hour. Accounting for fuel consumed during taxi, takeoff, climb, and descent, the total fuel consumption for the flight was estimated to be between 20 and 23 gallons. This suggests that about 15 to 18 gallons of usable fuel remained at the time of the accident. The weather conditions reported at the destination airport included a calculated relative humidity of 40% percent. Review of the icing probability chart contained within Federal Aviation Administration Special Airworthiness Information Bulletin CE-09-35 revealed the atmospheric conditions at the time of the accident were conducive to serious carburetor icing at glide power. Because the airplane was not recovered, and the wreckage could not be examined, the reason for the loss of engine power could not be determined. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Not determined-Not determined-(general)-(general)-Unknown/Not determined
Verbatim from NTSB's published report. Source file
NTSB_2025_ERA25LA216.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 ↗