NTSB CAROL · Event
Event MIA83LA108
Registry · N55AG
FAA Aircraft Registry record.
Make / Model
PIPER PA-30
Year of manufacture
1965 · 18 years old at event
TCDS
A1EA · PIPER AIRCRAFT INC
Engine
LYCOMING IO-320-B1A (160 hp)
Seats / Engines
6 seats · 2 engines
Last airworthiness date
20100419
ADS-B equipped
Yes — Mode-S A6FD19
Registrant of record
AIRCRAFT GUARANTY CORP TRUSTEE
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Factual narrative
THE ACFT DITCHED IN THE ATLANTIC OCEAN 5 MILES EAST OF PALM BEACH FL AFTER AN ELECTRICAL FIRE AND ENGINE FAILURE. THE PILOT SAID HE DEPARTED BOCA RATON AT 1950 EST. A FEW MINUTES LATER HE EXPERIENCED AN ELECTRICAL FIRE AND ELECTRICAL FAILURE. ABOUT 2 MINUTES LATER THE ENGINE QUIT. HE TRIED A RESTART WHICH WAS UNSUCCESSFUL AND DITCHED THE ACFT IN THE OCEAN WATER WHERE HE WAS RESCUED BY A FISHING BOAT. THE ACFT SANK AND WAS NOT RECOVERED. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1983_MIA83LA108.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 (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…
Browse the full corpus — academia portal ↗