ERA12CA042
2011-10-18 · Massey, Maryland, United States · Minor · 1 aircraft · Status: Completed
Airport MD1
Current FAA registration · N103ST
- Make / Model
- MOYES BAILEY DRAGONFLY
- Year of manufacture
- 1992 · 19 years old at event
- Engine
- ROTAX 582UL DCDI (65 hp)
- Seats / Engines
- 2 seats · 1 engine
- Last airworthiness date
- 20071117
- ADS-B equipped
- Yes — Mode-S A0117B
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot did not maintain airspeed during approach to landing, which resulted in an aerodynamic stall.
Factual narrative
The pilot stated that this was his first time flying the light sport airplane and just completed the first landing. He was getting familiarized with the airplane’s flight and landing characteristics. On the second landing, he permitted the airspeed low and the airplane stalled just prior to touchdown. A witness observed the airplane as it was approaching to land, its right wing dropped, impacting the ground. It then spun towards the right before the nose section impacted the ground; incurring substantial damage. The pilot stated there were no mechanical failures or malfunctions of the airplane or any of its systems prior to the accident. The pilot stated that this was his first time flying the light sport airplane, and he was getting familiarized with the airplane’s flight and landing characteristics. He completed one uneventful landing. On the second landing, he did not maintain airspeed, and the airplane stalled just before touchdown. A witness reported that, as the airplane was approaching to land, its right wing dropped and impacted the ground. The airplane then spun toward the right before the nose section impacted the ground and sustained substantial damage. The pilot stated that there were no mechanical failures or malfunctions of the airplane or any of its systems prior to the accident. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
- C Personnel issues-Action/decision-Action-Incorrect action performance-Pilot - C
Verbatim from NTSB's published report. Source file
NTSB_2011_ERA12CA042.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.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
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Related research
Matched on aircraft type or causal vocabulary (stall). All research papers
- Embry-Riddle Scholarly Commons 2021 · Journal article (IJAAA) Aerodynamic characterization of bio-mimicked pleated dragonfly aerofoil
The work inspired by the dragonfly wing corrugation positioned at the front wing's radius section lying at 40% of the total wingspan of forewing from the root section.
- 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…