MIA90FA071
1990-02-14 · ROSELAND, Florida, United States · None · 1 aircraft · Status: Completed
Airport X26
Aircraft involved
Probable cause & findings
THE ENGINE FAILURE DUE TO FUEL STARVATION CAUSED BY A NEEDLE VALVE IN THE CARBURETOR WHICH ALLOWS FUEL TO ENTER THE CARBURETOR BOWL, STUCK IN THE CLOSED POSITION FOR UNDETERMINED REASONS RESULTING IN THE FORCED LANDING.
Factual narrative
WHILE DESCENDING THROUGH 5,500 FROM 8,500 FT, PLT REPORTED THAT THE ENG LOST POWER. HE LEVELED OFF AT THE ALT & ATTEMPTED TO CORRECT THIS BUT WAS UNABLE. HE ELECTED TO CONTINUE TOWARD THE DEST BUT AFTER BEING ADVISED BY MIAMI CENTER THAT THE FLT WOULD NOT MAKE IT, ELECTED TO DIVERT TO AN ALTERNATE ARPT THAT WAS CLOSER. THE FLT WAS UNABLE TO LAND THERE. PLT ELECTED TO LAND ON A RD SHORT OF THE ARPT & DURING THE LANDING ROLL, THE ACFT COLLIDED WITH TREES, A FENCE & CAME TO REST WITH THE RT WING SEPARATED. AN ALTERNATE FUEL SUPPLY WAS CONNECTED FOR THE ENG RUN. AFTER IT STARTED IT WOULD ONLY RUN IF THE THROTTLE WERE PUMPED. WHILE IT WAS RUNNING, A MECHANIC TAPPED THE CARBURETOR BOWL AREA. THE ENG THEN OPERATED NORMALLY. CARBURETOR WAS REMOVED FOR FURTHER EXAM. EXAM OF IT REVEALED THE MOLDED CELLULAR FLOAT ABSORBED FUEL WHICH ALLOWED EXCESS FUEL INTO THE CARBURETOR BOWL. THE NEEDLE VALVE WAS EXAM. NO DETERMINATION COULD BE MADE AS TO WHY IT STUCK IN THE CLOSED POSITION AS INDICATED DURING THE ENG RUN. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1990_MIA90FA071.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
Matched on aircraft type or causal vocabulary (fuel starvation, engine failure). All research papers
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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.
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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…