NTSB CAROL · Event
Event ATL99LA042
Aircraft involved
Probable cause & findings
The loss of engine power for undetermined reasons.
Factual narrative
On January 13, 1999, at 1020 Eastern Standard Time, a Cessna 210N, N5458A, ditched in the Atlantic Ocean 300 yards off the coast of Hallandale Beach, Florida. The airplane was owned by K.P. Cleary & Associates, Inc., and operated under the provisions of Title 14 CFR Part 91, and visual flight rules. Visual meteorological conditions prevailed at the accident site and no flight plan was filed for the personal flight. The private pilot received minor injuries and the airplane sustained substantial damage. The airplane departed Fort Lauderdale International Airport (FLL) in Fort Lauderdale, Florida, at 1010, destined for Marathon, Florida. According to the pilot, preflight inspection of the airplane revealed approximately 55 gallons of fuel on board and no abnormalities were noted during the engine run-up. The pilot stated, while climbing through 1500 feet MSL, the engine RPM began to fluctuate as the throttle was increased. The pilot informed Miami Approach Control of the engine problem and was given clearance to fly direct to FLL. According to the pilot, after the engine stopped running, he switched tanks multiple times while working through the restart checklist. The pilot stated, at this point the airspeed had diminished to stall speed and the airplane was at a very low altitude. The pilot extended the flaps and ditched the airplane in the Atlantic Ocean. The pilot was retrieved from the water by the Hollywood Beach Patrol. The airplane sank in 30 feet of water. According to a Federal Aviation Administration (FAA) inspector who examined the wreckage after its recovery, the airplane was substantially damaged. The post recovery inspection of the engine revealed no significant mechanical problems. The FAA inspector also noted that, the engine was removed from the wreckage and ran at operating power settings for more than ten minutes. According to the pilot, preflight inspection of the airplane revealed approximately 55 gallons of fuel on board and no abnormalities were noted during the engine run-up. While climbing through 1500 feet MSL, the engine RPM began to fluctuate as the throttle was increased. After advising approach control of his engine problem, the pilot was given clearance to the departure airport. After the engine stopped running, the pilot switched tanks multiple times, altitude decreased and the airspeed diminished to stall speed. The pilot extended the flaps and ditched the airplane in the Atlantic Ocean. The airplane sank in 30 feet of water. According to a Federal Aviation Administration (FAA) inspector, post recovery inspection of the engine revealed no significant mechanical problems. The FAA inspector also noted, the engine was removed from the wreckage and ran at a sufficient power setting for more than ten minutes. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1999_ATL99LA042.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 (stall). 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 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
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