NTSB CAROL · Event
Event ERA11CA304
Registry · N619LM
FAA Aircraft Registry record.
Make / Model
COSTRUZIONI AERONAUTICHE TECNA P2002 SIERRA
Year of manufacture
2008 · 3 years old at event
Engine
ROTAX 912ULS SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20080719
ADS-B equipped
Yes — Mode-S A81133
Registrant of record
ARENA ALBERT
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot's improper flare which resulted in a hard landing, and the flight instructor's lack of remedial action.
Factual narrative
According to the flight instructor, the student pilot was landing on the 2,903-foot by 60-foot runway 29 with winds from 320 degrees true at 4 knots. The approach was "seemingly normal," with the airplane trimmed for an approach airspeed of 62 knots, and configured with approximately one-half flaps. About 15 to 20 feet above the runway, with no pre-stall indication or buffeting noted, the airplane suddenly dropped, then impacted the runway. The airplane then veered off the left side of the runway, and the right wing was substantially damaged when it impacted a precision approach path indicator (PAPI) stanchion. The flight instructor did not report any preexisting mechanical anomalies with the airplane. According to the flight instructor, the student pilot was landing with the airplane trimmed for an approach airspeed of 62 knots and configured with approximately one-half flaps. About 15 to 20 feet above the runway, with no prestall indication or buffeting noted, the airplane suddenly dropped, then impacted the runway. The airplane veered off the left side of the runway, and the right wing was substantially damaged when it impacted a precision approach path indicator stanchion. The flight instructor did not report any preexisting mechanical anomalies with the airplane. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- C Personnel issues-Action/decision-Action-Lack of action-Student pilot - C
- C Personnel issues-Action/decision-Action-Lack of action-Instructor/check pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Airspeed-Not attained/maintained - C
Verbatim from NTSB's published report. Source file
NTSB_2011_ERA11CA304.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…
Browse the full corpus — academia portal ↗