NTSB CAROL · Event
Event MIA97LA215
Aircraft involved
Probable cause & findings
Failure of the aircraft to maintain altitude for undetermined reasons following loss of power in one engine.
Factual narrative
On July 24, 1997, about 1620 eastern daylight time, a Beech 65, N816Q, registered to M R Aircraft Sales and Rental, Inc., ditched in the Atlantic Ocean following loss of power in one engine, while on a Title 14 CFR Part 91 personal flight, from Miami, Florida, to Kingston, Jamaica. Visual meteorological conditions prevailed at the time and an instrument flight rules flight plan was filed. The aircraft was not recovered and presumed to be destroyed. The commercial-rated pilot, commercial-rated second pilot, and three passengers were not injured. The flight originated from Miami, Florida, the same day, about 1501. The pilot-in-command stated that about 1 hour after takeoff, at 9,000 feet, the left engine failed. They turned toward Bain Airport, Andros Island, Bahamas. The passengers were briefed. The airplane would not maintain altitude on one engine and was ditched about 25 miles from the Andros Island shoreline at about 1620. They were rescued the next morning about 0745. The second pilot stated he was flying the aircraft from the left seat and that he was the owner of the aircraft. The takeoff and climb to the cruising altitude of 9,000 feet was normal. About 15 minutes after reaching the cruising altitude, while near "URSUS" intersection on airway "A-509", the left engine quit. Attempts to restart the engine were unsuccessful and the engine was shut down and the propeller was feathered. The aircraft would not maintain altitude and entered a 500 feet per minute rate of descent. He turned to the closest airport, Bain Airport, which was about 80 miles to the east-northeast. The aircraft continued to descend and they ditched in the ocean about 50 miles from the Bain Airport. After ditching, he and the occupants exited the aircraft uninjured and boarded a raft. They were rescued the following morning. The second pilot stated that at the beginning of taxi for takeoff the aircraft weighed 7,790 pounds and that the maximum allowable takeoff weight is 7,700 pounds. The previous owner of the aircraft stated the aircraft logbooks had been lost before he purchased the aircraft. Information he had showed the aircraft had accumulated about 4,300 total flight hours and that each engine had about 450 flight hours over the recommended overhaul time. About 1 hour after departure and 15 minutes after reaching the cruising altitude of 9,000 feet, the left engine quit. The flight crew feathered the left propeller and turned toward the closest airport which was 80 miles away. The aircraft would not maintain altitude and entered a 500 foot per minute descent. About 20 minutes after engine failure the aircraft was ditched in the ocean about 50 miles from the closest airport. The flight crew and passengers were rescued the following morning and the aircraft was not recovered. The second pilot and owner of the aircraft stated the aircraft was about 90 pounds over the maximum allowable weight at the time of departure. The previous owner of the aircraft stated that both engines had exceeded the recommended overhaul time by about 450 flight hours. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1997_MIA97LA215.txt.
Findings + structured fields enriched from FAA avall.mdb.
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Related research
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Academic papers and agency reports matching this event's aircraft type or causal vocabulary (engine failure). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- arXiv 2022 · arXiv preprint
Multi-level Adaptation for Automatic Landing with Engine Failure under Turbulent Weather
This paper addresses efficient feasibility evaluation of possible emergency landing sites, online navigation, and path following for automatic landing under engine-out failure subject to turbulent wea…
- NASA NTRS 2019 · Conference Paper
Simulation of Liquid Rocket Engine Failure Propagation Using Self-Evolving Scenarios
Traditional probabilistic risk assessment approaches often require failure scenarios to be explicitly defined through event sequences that are then quantified as part of the integrated analysis.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techiques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Conference Paper
Rocket engine failure detection using system identification techniques
The theoretical foundation and application of two univariate failure detection algorithms to Space Shuttle Main Engine (SSME) test firing data is presented.
- NASA NTRS 2019 · Technical Memorandum (TM)
A simulator investigation of engine failure compensation for powered-lift STOL aircraft
A piloted simulator investigation of various engine failure compensation concepts for powered-lift STOL aircraft was carried out at the Ames Research Center.
- Semantic Scholar 2019 · Article (AIAA Scitech 2019 Forum)
Impact of Engine Failure Constraints on the Initial Sizing of Hybrid-Electric GA Aircraft
Potential advantages of hybrid-electric aircraft are fuel savings, lower emissions, and reduced noise. Since these aircraft generally apply multiple power sources, they can also be designed to sustain…
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