NYC06LA055
2006-01-20 · Churchville, Maryland, United States · Serious · 1 aircraft · Status: Completed
Airport 0W3
Current FAA registration · N1923S
- Make / Model
- RENQUIST JOHN H STARDUSTER TOO SA300
- Year of manufacture
- 1984 · 22 years old at event
- Engine
- LYCOMING I0360 SER A&C (200 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 19981021
- ADS-B equipped
- Yes — Mode-S A1726B
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain adequate airspeed during takeoff, which resulted in an inadvertent stall.
Factual narrative
On January 20, 2006, at 1707 eastern standard time, an amateur-built Starduster SA300, N1923S, was substantially damaged when it impacted the ground, after takeoff from the Harford County Airport (0W3), Churchville, Maryland. The certificated commercial pilot was seriously injured. Visual meteorological conditions prevailed for the personal flight destined for the Martin State Airport (MTN), Baltimore, Maryland. A visual flight rules (VFR) flight plan was filed, and the flight was conducted under 14 CFR Part 91. According to a Federal Aviation Administration (FAA) inspector who examined the airplane after the accident, witnesses observed the airplane "climbing like a rocket" during takeoff from runway 28. As the airplane reached an altitude of approximately 70 feet, it banked to the left, then to the right, and then descended to the ground. The airplane impacted the ground in a nose-low attitude, resulting in substantial damage. Examination of the airplane by the FAA inspector revealed no mechanical deficiencies with the airframe or engine. The pilot failed to respond to numerous requests for his statement regarding the accident. The winds reported at an airport 18 miles to the southwest, at 1645, were from 110 degrees at 6 knots. Witnesses at the Harford Airport reported that at the time of the accident, there was a 5-8 knot, "90-degree crosswind" for runway 28. Witnesses observed the airplane "climbing like a rocket" during takeoff. As the airplane reached an altitude of approximately 70 feet, it banked to the left, then to the right, and then descended to the ground. The airplane impacted the ground in a nose-low attitude, resulting in substantial damage. Examination of the airplane revealed no mechanical deficiencies with the airframe or engine. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2006_NYC06LA055.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
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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…