NTSB CAROL · Event
Event ATL02LA037
Aircraft involved
Probable cause & findings
The loss of engine power for undetermined reasons.
Factual narrative
On January 13, 2002, at 1700 central standard time, a Stinson 108M, N9315K, experienced a loss of engine power on the initial takeoff/climb from Roy E. Ray Airport in Bayou La Batre, Alabama. The airplane, registered to Consolidated-Vultee, was operated by the pilot under the provisions of Title 14 CFR part 91. The personal flight was enroute from Bayou La Batre, Alabama to St. Elmo, Alabama. Visual meteorological conditions prevailed at the time of the accident and no flight plan was filed. The private pilot received serious injuries and the airplane sustained substantial damage. The pilot stated there were 20 gallons of fuel on board at takeoff. According to the pilot, the engine lost power at 400 feet above the ground during the climb out. The pilot stated that he established glide at 65-70mph and attempted an engine restart unsuccessfully. The pilot executed a left turn and collided with power lines approximately 35 above ground. The airplane subsequently came to rest in a nearby ditch about 400 feet from the end of the departure runway 36. A review of weather data showed conditions favorable for the formation of carburetor icing; the temperature was 57 degrees Fahrenheit and the dew point was 42 degrees Fahrenheit. Tests were performed on both magnetos, they both operated within normal parameters. A functional check of the engine was performed; the power was checked at 2700 rpm and results indicated that the engine ran smoothly at full power and at idle. Oil pressure was normal during the functional check. The functional check of the engine failed to disclose a mechanical malfunction or component failure. A Stinson 108M, experienced a loss of engine power on the initial takeoff/climb from Roy E. Ray Airport in Bayou La Batre, Alabama. According to the pilot, the engine lost power at 400 feet above the ground during the climb out. The pilot executed a left turn and collided with power lines approximately 35 above ground. The airplane came to rest in a nearby ditch about 400 feet from the end of the departure runway 36. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_ATL02LA037.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 ↗