MIA01LA149
2001-05-30 · Greensboro, North Carolina, United States · None · 1 aircraft · Status: Completed
Airport W88
Current FAA registration · N1669G
- Make / Model
- CHAMPION 7ECA
- Engine
- LYCOMING 0-235 SERIES (115 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19681003
- ADS-B equipped
- Yes — Mode-S A10B92
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the pilot's failure to maintain airspeed during takeoff/initial climb, which resulted in an inadvertent stall, an uncontrolled descent, and collision with trees.
Factual narrative
On May 30, 2001, about 1954 eastern daylight time, a Champion 7ECA, N1669G, registered to Omni Aviation Inc., and operated as a Title 14 CFR part 91 personal flight, crashed into trees during takeoff/initial climb at Air Harbor Airport, Greensboro, North Carolina. Visual meteorological conditions prevailed, and no flight plan was filed. The airline transport-rated pilot and one pilot-rated passenger were not injured, and the aircraft incurred substantial damage. The flight was originating at the time of the accident. The pilot stated that it had been a normal takeoff, with all engine and flight indications being normal. The pilot further stated that he had rotated about 800 feet down the runway, and had climbed to about 100 feet, when the aircraft suddenly made an uncommanded left turn. He said he tried to recover, but there was no response to control inputs, and the aircraft impacted the tops of pine trees, coming to rest at a height of about 30 feet into the trees. The pilot stated that he supposed that inadvertent rudder input or p-factor caused the left turn, due to slow airspeed, prior to stall. The pilot reiterated that there had not been any mechanical failure or malfunction to the aircraft's engine, or to any of the aircraft systems prior to the accident. The pilot stated that he had rotated about 800 feet down the runway, and climbed about 100 feet, when the aircraft suddenly made an uncommanded left turn and came to rest in some trees. The pilot further stated that he supposed that inadvertent rudder input or p-factor caused the left turn due to slow airspeed prior to stall. He said there had not been any mechanical failure or malfunction to the aircraft or any of its systems prior to the accident. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2001_MIA01LA149.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
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Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- 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…