NTSB CAROL · Event
Event MIA95LA136
Registry · N6188F
FAA Aircraft Registry record.
Make / Model
CESSNA A150L
Engine
CONT MOTOR 0-200 SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
19730816
ADS-B equipped
Yes — Mode-S A80FEC
Registrant of record
SKY HIGH ADVENTURES LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
THE DUAL STUDENT'S IMPROPER USE OF THE RUDDER FOLLOWING A LEFT SWERVE DURING LANDING ROLLOUT WHICH PREVENTED THE FLIGHT INSTRUCTOR FROM REGAINING DIRECTIONAL CONTROL.
Factual narrative
On May 25, 1995, about 1415 eastern daylight time, a Cessna A150L, N6188F, registered to a private individual, veered left and separated the right main landing gear during landing at Kendall-Tamiami Executive Airport, Miami, Florida, while on a 14 CFR Part 91 instructional flight. Visual meteorological conditions prevailed at the time and no flight plan was filed. The aircraft received substantial damage and the commercial-rated pilot/flight instructor and dual student were not injured. The flight originated from Miami, Florida, on May 25, 1995, about 1330. The flight instructor stated the aircraft had been modified to remove the nose landing gear and install a tail landing gear. The student performed a normal landing and they were rolling down the runway with the tailwheel on the runway, when the aircraft began to veer to the left. He took control of the aircraft and attempted to correct the left veer. The student appeared to have become confused and applied full left rudder and his corrections to the right were unsuccessful. As the aircraft turned further left the right main landing gear separated at the attach point due to the excessive loading. The right wing contacted the runway and the aircraft came to rest. Postaccident examination of the aircraft by FAA inspectors showed no evidence of precrash failure or malfunction of the tailwheel steering system or right main landing gear. THE AIRCRAFT SWERVED TO THE LEFT DURING LANDING ROLLOUT. WHEN THE FLIGHT INSTRUCTOR ATTEMPTED TO TAKE CONTROL AND CORRECT FOR THE SWERVE THE STUDENT WAS HOLDING FULL LEFT RUDDER. THE AIRCRAFT TURNED TO THE LEFT AND THE RIGHT MAIN LANDING GEAR COLLAPSED DUE TO OVERLOAD. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_1995_MIA95LA136.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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