NTSB CAROL · Event
Event MIA93LA149
Registry · N8962L
FAA Aircraft Registry record.
Make / Model
BOEING 737-8
Year of manufacture
2025
TCDS
A16WE · THE BOEING CO
Engine
CFM INTL LEAP-1B28 SER
Seats / Engines
175 seats · 2 engines
Last airworthiness date
20250620
ADS-B equipped
Yes — Mode-S AC5E47
Registrant of record
SOUTHWEST AIRLINES CO
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
PREMATURE LIFT OFF BY THE PILOT DURING TAKEOFF.
Factual narrative
On July 4, 1993, about 0906 eastern daylight time, a Grumman AA-1B, N8962L, registered to the pilot, William L. Hines, was substantially damaged during an aborted takeoff from the Ocala Municipal Airport, Ocala, Florida, while on a 14 CFR Part 91 personal flight. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local flight. The private pilot sustained minor injuries. The flight was originating at the time of the accident. The pilot stated that during the initial climb, the aircraft shuddered as if it would fall apart. The shuddering stopped after he decreased the angle of attack; and the engine did respond to throttle input. He again initiated a climb and the shuddering began again. He aborted the takeoff and while maneuvering to avoid obstacles at the departure end of the runway, the airplane stalled and landed hard on grass. The nose and right main landing gears collapsed. He further stated that the shuddering was similar to that encountered when performing stalls and that he did not hear any unusual engine sounds. As a result of the accident, the fuel tanks were damaged but the remaining fuel in them, the carburetor, and electric fuel pump were checked for water; none was found. A slight amount of sediment was found. An A & P mechanic who examined the engine stated that it was "intact." The magnetos were removed, rotated by hand, which revealed that they produced more than sufficient spark. THE FLIGHT DEPARTED AND DURING THE INITIAL CLIMB, THE PILOT REPORTED THAT THE AIRPLANE SHUDDERED AS IF IT WOULD FALL APART. THE SHUDDERING STOPPED WHEN HE DECREASED THE ANGLE OF ATTACK; AND THE ENGINE DID RESPOND TO THROTTLE INPUT. HE AGAIN INITIATED A CLIMB AND THE SHUDDERING STARTED AGAIN. HE ABORTED THE TAKEOFF AND WHILE MANEUVERING TO AVOID OBSTACLES PAST THE DEPARTURE END OF THE RUNWAY, THE AIRPLANE STALLED AND LANDED HARD ON THE GRASS. THE NOSE AND RIGHT MAIN LANDING GEARS COLLAPSED. HE FURTHER STATED THAT THE SHUDDERING WAS SIMILAR TO THAT ENCOUNTERED WHILE PERFORMING STALLS AND THAT HE DID NOT HEAR ANY UNUSUAL ENGINE SOUNDS. THE FUEL SYSTEM WAS CHECKED FOR WATER; NONE WAS FOUND. EXAMINATION OF THE ENGINE REVEALED NO EVIDENCE OF FAILURE OR MALFUNCTION. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1993_MIA93LA149.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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