NTSB CAROL · Event
Event MIA07CA096
Aircraft involved
Probable cause & findings
The pilot's failure to maintain directional control during landing.
Factual narrative
The pilot stated he flew a stabilized approach and had a normal touchdown. After touchdown the airplane veered to the left; he compensated with right rudder but got no response. As the airplane drifted to the left, he increased the right rudder inputs and also used right toe-brake but again got no response. Before exiting the runway he pulled the handbrake while applying hard right toe-brake. The aircraft did slow but didn't turn to the right. After exiting the runway the airplane overran the VASI light system and struck a row of runway lights. After which the airplane impacted an embankment and slid obliquely down the side of it. The airplane then impacted another embankment perpendicular to that one, shearing the nose-wheel, bending the prop and engine-cowl. The airplane then rolled to the left and the wing struck the ground, buckling the inboard side fuel tank bulkhead and partially shearing from the fuselage before it come to a stop. The pilot stated that the airplane's nose-wheel steering and braking performed normally prior to the accident flight. The responding FAA inspector stated that examination of the site indicated the airplane's touched down point was 25 yards from the end of the runway and 8 yards left of the centerline, and angled directly towards the second VASI light installation. Following the tire tracks it appears that the underside of the left wing impacted the VASI light. The pilot stated to the FAA inspector that there were no mechanical difficulties with the aircraft. The pilot stated that he flew a stabilized approach and had a normal touchdown. After touchdown the airplane veered to the left, and he compensated with right rudder but got no response. As the airplane drifted to the left, he increased the right rudder inputs and also used right toe-brake but again got no response. Before exiting the runway he pulled the handbrake while applying hard right toe-brake. The aircraft did slow but didn't turn to the right. After exiting the runway the airplane overran the VASI light system and struck a row of runway lights. After which the airplane impacted an embankment and slid obliquely down the side of it. The airplane then impacted another embankment perpendicular to that one, shearing the nose-wheel, bending the prop and engine-cowl. The airplane then rolled to the left and the wing struck the ground, buckling the inboard side fuel tank bulkhead and partially shearing from the fuselage before it come to a stop. The pilot stated that the airplane's nosewheel steering and brakes performed normally prior to the accident flight. The responding FAA inspector stated that examination of the site indicated that the airplane touchdown point was 25 yards from the end of the runway and 8 yards left of the centerline, and angled directly towards the second VASI light installation. Following the tire tracks it appears that the underside of the left wing impacted the VASI light. The pilot stated to the FAA inspector that there were no mechanical difficulties with the aircraft. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2007_MIA07CA096.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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