NTSB CAROL · Event
Event MIA01LA236
Aircraft involved
Probable cause & findings
an on ground fire that started in the engine due to an excessive fuel flow causing the engine to flood. A factor in this accident was the pilot-in-command did not follow all the emergency procedures for an engine fire during start.
Factual narrative
On June 14, 2001, about 1030 eastern daylight time, a Piper PA-28-161, N554HA, owned and operated by Venice Flying Service Inc., as a Title 14 CFR Part 91 test flight had an engine fire during taxi, and after landing at the Venice Airport, Venice, Florida. Visual meteorological conditions prevailed. No flight plan was filed. The airplane was substantially damaged. The airline transport rated-pilot reported no injuries. The flight had originated from the Venice Airport at 0930. According to the pilot, after landing and exiting the runway, "the engine stall[ed]. When I was trying to restart some smoke start[ed] to come out from the engine. I crank it a little bit longer then exit[ed] the airplane as it was burning." Note: The pilot operator handbook (POH) for the Piper PA-28-161 states, "...if fire continues more than a few seconds, the fire should be extinguished by the best avialable external means...the fuel selector valves should be "OFF" and the mixture at idle cut-off if an external fire extinguishing method is used." According to an FAA inspector, "…[the pilot's] first attempt to restart was unsuccessful. He cleared the engine by cranking with full throttle and the mixture in idle cutoff. On his second attempt to start the engine, the engine again failed to start, and upon seeing smoke, he ceased cranking the engine… The aircraft was positioned on the taxiway 90 degrees to the prevailing wind. As a result most of the fire damage is to the left side of the engine compartment." In addition, the inspector reported that the airplane had a 2-year history of "intermittent stalling problems after landing." The carburetor had been replaced on four occasions, including the day of the fire. The fuel and ignition systems had been checked repeatedly during troubleshooting and various repairs accomplished to include spark replacement, internal magneto timing, and fuel filter cleaning. The accident was never reported to the NTSB. An FAA inspector discovered the wreckage on October 26, 2001, during a routine inspection of the fixed base operator's facilities. During taxi after landing the airplane's engine stalled. The pilot's first attempt to restart was unsuccessful. He cleared the engine by attempting to restart with full throttle and the mixture in idle cutoff. On his second start attempt the engine again failed to start, and upon seeing smoke, he ceased cranking the engine, and exited the airplane… Most of the fire damage was to the left side of the engine compartment. The airplane had a 2-year history of intermittent stalling problems after landing. The carburetor had been replaced on four occasions, including the day of the fire. The fuel and ignition systems had been checked repeatedly during troubleshooting and various repairs accomplished to include spark replacement, internal magneto timing, and fuel filter cleaning. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_MIA01LA236.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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