MIA96LA214
1996-08-16 · PLANT CITY, Florida, United States · None · 1 aircraft · Status: Completed
Airport PCM
Current FAA registration · N7053F
- Make / Model
- CESSNA 150F
- Seats / Engines
- 2 seats · 1 engine
- ADS-B equipped
- Yes — Mode-S A969E8
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
a loss of engine power due to fuel contamination, resulting in a forced landing, and subsequent nose over. A factor in this accident was an inadequate aircraft pre-flight
Factual narrative
On August 16, 1996, about 1910 eastern daylight time, a Cessna 150F, N7053F, registered to a private owner, operating as a 14 CFR Part 91, personal flight, crashed in the vicinity of Plant City, Florida. Visual meteorological conditions prevailed and no flight plan was filed. The airplane was substantially damaged. The private pilot was not injured. The flight had taken off from runway 9, and had climbed to an altitude of about 150 feet mean sea level, when the airplane's engine lost power. The pilot elected to make an off airport landing, turned the airplane to the left to clear trees, touched down in a field, and nosed over. Examination of the wreckage by the FAA revealed that 2 ounces of fuel was drained from the gascolator, and about 3/4 of an ounce of the fuel was water. In addition, 1 ounce of water was drained from the carburetor bowl. The engine rotated freely and no discrepancies were found. According to the FAA inspector's statement, "...[this] aircraft [had] flown only 5 hours in over 12 months, [and was] not fueled since sometime in February 1996, possible engine failure due to fuel contamination." The flight had taken off from runway 9, and had climbed to an altitude of about 150 feet mean sea level, when the airplane's engine lost power. The pilot elected to make an off airport landing, turned the airplane to the left to clear trees, touched down in a field, and nosed over. Examination of the wreckage revealed that 2 ounces of fuel was drained from the gascolator, about 3/4 of an ounce of the fuel was water, and 1 ounce of water was drained from the carburetor bowl. The engine rotated freely and no discrepancies were found. In addition, this airplane had flown only 5 hours in the past 12 months, and had not been fueled, before this flight, since sometime in February 1996. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1996_MIA96LA214.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type or causal vocabulary (fuel contamination, engine failure). All research papers
- 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…