NTSB CAROL · Event
Event MIA04LA120
Registry · N45TT
FAA Aircraft Registry record.
Make / Model
AVIAT AIRCRAFT INC A-1C-200
Year of manufacture
2010
Engine
LYCOMING IO-360-A1D6D (200 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20100105
ADS-B equipped
Yes — Mode-S A5717E
Registrant of record
DIFCO LEASING LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's inadequate planning/decision and his failure to maintain airspeed which resulted in fuel exhaustion and an inadvertent stall.
Factual narrative
On August 12, 2004, about 1515 central daylight time, N45TT, a Beech King Air 65-A90, registered to and operated by Eclipse Enterprises Inc., as a Title 14 CFR part 91 business flight, crashed while returning to land at Ferguson Airport, Pensacola, Florida. Visual meteorological conditions prevailed, and no flight plan was filed. The commercial-rated pilot, and one passenger received minor injuries, and the airplane incurred substantial damage. The flight was originating at the time of the accident. The pilot stated that he was flying the accident airplane from Ferguson Airport, Pensacola, Florida, to Jack Edwards Airport, Gulf Shores, Alabama, to refuel, and during the takeoff, immediately after rotating, he tapped the brakes, raised the landing gear, and about 3 to 4 seconds later the right engine ceased operating. He stated that he was sure the engine ceased operating due to fuel exhaustion, because he knew the airplane was low on fuel. After the right engine ceased operating, the airplane drifted right, and he inputted full left rudder, and placed left wing down to correct. He then confirmed that the right engine was spooling down, and feathered the propeller on the right engine. He then started a turn to the side of the operating engine to return to the airport. As he rolled the wings level, he said the airplane started to climb, so he reduced power after clearing the trees, and at that time the rate of descent increased. He said the airplane's speed was about 80 knots and the stall warning light began flickering on and off, and it also felt as if he was falling out of the sky. The pilot added full power which caused the nose to veer radically to the right, and the airplane descended, heading toward some T-hangars. He kept the landing gear retracted, and attempted to land the airplane on its belly to keep from colliding with the hangar. In doing so, both the wing and nose of the aircraft struck the ground. The pilot reported that there had been no indications of any mechanical failures or malfunctions of the airplane or any of its systems. The pilot stated that he was proceeding to a nearby airport to refuel, and during the takeoff from his departure airport, about 3 to 4 seconds after rotating, the right engine ceased operating due to fuel exhaustion. He said that the airplane drifted to the right, and he feathered the right propeller and turned to the right in order to return to the runway. After leveling, he said the airplane started to climb so he reduced power, and as he did so the airspeed dropped to 80 knots, and the stall warning light was activated. He said he added full power to recover, and the aircraft veered radically to the right in the direction of the hangars. Keeping the landing gear in the up position, he said he performed a belly landing and the airplane incurred damage. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2004_MIA04LA120.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, fuel exhaustion). 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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