NTSB CAROL · Event
Event CEN23LA216
Registry · N133LS
FAA Aircraft Registry record.
Make / Model
REMOS AIRCRAFT GMBH G-3/600
Year of manufacture
2007 · 16 years old at event
Engine
ROTAX 912ULS SERIES (100 hp)
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20071212
ADS-B equipped
Yes — Mode-S A08761
Registrant of record
LSA-MIDWEST LLC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The student pilot’s improper flight control inputs and the flight instructor’s delayed remedial action during takeoff, which resulted in a runway excursion and impact with terrain.
Factual narrative
The flight instructor and student pilot intended to complete a cross-country flight. During the takeoff roll, the student pilot pitched the nose up to 15° then lowered it to 5° upon request of the instructor. As the takeoff roll continued, the student abruptly applied right rudder and again increased the pitch attitude. The airplane veered to the right and became airborne off the right side of the runway. The instructor took control of the airplane as it began to stall about 20 ft. above ground level. The airplane bounced and the propeller struck the ground, then it porpoised, and came to rest in a field about 1,000 ft. from the runway. The landing gear collapsed, and the elevator sustained substantial damage. The flight instructor reported that there were no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. 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).
- — Personnel issues-Action/decision-Action-Delayed action-Instructor/check pilot
- — Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained
- — Personnel issues-Action/decision-Action-Incorrect action performance-Student/instructed pilot
- — Personnel issues-Task performance-Use of equip/info-Aircraft control-Flight crew
Verbatim from NTSB's published report. Source file
NTSB_2023_CEN23LA216.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, runway excursion). 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 …
- SKYbrary (Eurocontrol) 2024 · SKYbrary article
Runway Excursion — SKYbrary Knowledge Base
SKYbrary runway excursion review — RE-OE (overruns) + RE-LO (lateral). Risk drivers: long landing, high approach speed, contaminated surface, tailwind, mis-set autobrakes.
- 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…
Browse the full corpus — academia portal ↗