NTSB CAROL · Event
Event MIA02LA105
Aircraft involved
Probable cause & findings
The flight instructor's inadequate supervision of the dual student and failure to take prompt remedial action, resulting in a collision with a tree, a subsequent loss of control, and collision with the ground.
Factual narrative
On June 4, 2002, about 1230, eastern daylight time, a Cessna 150M, N63591, registered to, and operated by Ormond Beach Aviation Inc., as a Title 14 CFR Part 91 instructional flight, crashed during takeoff/initial climb from the Ormond Beach Municipal Airport, Ormond Beach, Florida. Visual meteorological conditions prevailed, and no flight plan was filed. The aircraft incurred substantial damage, and the commercial-rated flight instructor and dual student received minor injuries. The flight was originating at the time of the accident. The flight instructor stated that he and his student were initiating a flight, so his student could practice soft and short field takeoffs and landings. He stated that the takeoff and initial climb were uneventful, with the engine developing full power, and that during the climb the student pitched the aircraft up excessively, and the airspeed decayed to near the stall speed. The instructor further stated that he then took control of the aircraft to avert a departure stall, pitching down to attain sufficient airspeed, but the aircraft would not climb sufficiently. As they approached some trees at the end of the runway, he said he steered the aircraft toward an area of lower trees, extending the flaps to 40 degrees, in an attempt to balloon over the trees, but the left main landing gear became entangled in a tree. The aircraft flipped over, coming to rest nearly inverted at the base of a tree, incurring substantial damage. An FAA Inspector responded to the accident, and conducted an examination of the accident aircraft. The inspector noted that there was extensive structural damage to the aircraft, and stated that he did not find evidence of any preaccident failures or malfunctions to the aircraft or any of its systems which would have caused the accident. The flight instructor stated that the takeoff and initial climb were uneventful, with the engine developing full power, and that during the climb the student pitched up excessively, and the airspeed decayed to near the stall speed. He said he then took control of the aircraft to avert a departure stall, and tried to clear trees at the end of the runway, steering the aircraft toward an area of lower trees, and extending the flaps to forty degrees in an attempt to balloon over the trees, but the left main landing gear became entangled in a tree, and the aircraft crashed incurring substantial damage. An FAA Inspector conducted a postaccident examination of the aircraft and stated that he did not find evidence of any preaccident failures or malfunctions to the aircraft or any of its systems which would have caused the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2002_MIA02LA105.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, loss of control). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Semantic Scholar 2016 · Article (Interacción)
Trajectory Recovery System: Angle of Attack Guidance for Inflight Loss of Control
This paper describes the design and development of an ecological display to aid pilots in the recovery of an In-Flight Loss of Control event due to a Stall (ILOC-S).
- NTSB Aircraft Accident Reports 2010 · Accident report
Loss of Control on Approach — Colgan Air Flight 3407
Colgan Air 3407 / Continental Connection (Q400) Buffalo NY, February 12, 2009 — 50 fatalities. Definitive investigation of the Colgan 3407 stall-stick-pusher crash on approach to Buffalo.
- 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 …
- Embry-Riddle Scholarly Commons 2025 · Journal article (JAAER)
A Scoping Review of Aviation Loss of Control Inflight Research
Loss of control – inflight (LOC-I) contributes to aircraft accidents at unacceptably high rates. Significant industry efforts and research have aimed to improve LOC-I prevention, detection, and recove…
- arXiv 2025 · arXiv preprint
Quadratic Programming Approach to Flight Envelope Protection Using Control Barrier Functions
Ensuring the safe operation of aerospace systems within their prescribed flight envelope is a fundamental requirement for modern flight control systems.
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Loss of Control In-Flight (LOC-I) — SKYbrary Knowledge Base
SKYbrary comprehensive knowledge-base entry on Loss of Control In-Flight — definitions, contributing factors, accident case studies (Air France 447, Colgan 3407), and prevention strategies.
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