NTSB CAROL · Event
Event CEN13LA418
Registry · N613LD
FAA Aircraft Registry record.
Make / Model
MARK MARINO BENOIST TYPE XIV
Engine
AMA/EXPR UNKNOWN ENG
Seats / Engines
2 seats · 1 engine
Last airworthiness date
20130627
ADS-B equipped
Yes — Mode-S A7FAE1
Registrant of record
EAA AVIATION FOUNDATION INC
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
The pilot's failure to maintain control of the seaplane during its initial flight test. Contributing to the accident was the pilot's overall lack of flight experience in the seaplane.
Factual narrative
On July 16, 2013, at 1130 central daylight time, an experimental amateur-built Marino model Benoist Type XIV seaplane, N613LD, was substantially damaged when it impacted water shortly after takeoff from Superior Bay near Duluth, Minnesota. The private pilot was not injured. The seaplane was registered to and operated by Duluth Aviation Institute, under the provisions of 14 Code of Federal Regulations Part 91, without a flight plan. Day visual meteorological conditions prevailed for the local flight test that departed Sky Harbor Airport (KDYT), Duluth, Minnesota, about 1110. The accident occurred during the first flight since the seaplane was issued an experimental airworthiness certificate on June 27, 2013. The seaplane was a replica of a 100 year old design. The pilot reported that the seaplane had accumulated 3.7 hours of water operations before he attempted the accident flight. Additionally, he stated that there were no anomalies with the seaplane during the two water taxi runs that were completed immediately before the accident takeoff. He reported that his test plan was to achieve liftoff and then fly 1-2 feet above the water for a couple hundred yards before landing. The pilot stated that during the takeoff run he increased engine power, from 3,000 rpm to 4,000 rpm, after which the seaplane became airborne within a few seconds and unexpectedly entered a high climb angle. He made a pitch reduction, but the seaplane responded quicker than he expected and a pitch increase was subsequently required to avoid a collision with the water. The seaplane ultimately climbed to about 30 feet above the water before the pilot initiated a descent for a landing. The pilot reported that he “could not control the landing” and that the seaplane impacted the water in a nose low and right wing low attitude. The forward fuselage and wings sustained substantial damage during the impact. The pilot extricated himself from the wreckage and was recovered by his support crew following in a chase boat. The pilot reported that there were no mechanical anomalies with the seaplane during the accident flight. In addition, he noted that his overall lack of flight experience in the seaplane contributed to the accident. At 1134, the KDYT automated surface observing system reported the following weather conditions: wind 090 degrees true at 3 knots, visibility 10 miles, sky clear, temperature 19 degrees Celsius, dew point 17 degrees Celsius, altimeter setting 30.16 inches of mercury. The accident occurred during the first flight after the seaplane was issued an experimental airworthiness certificate. According to the pilot, the seaplane was a replica of a 100-year-old design and had very unconventional controls. The pilot reported that his initial flight test plan was to take off and then fly 1-2 feet above the water for a couple hundred yards before landing again. However, he stated that immediately after liftoff, the seaplane unexpectedly pitched up steeply. The pilot reduced the seaplane’s pitch attitude to avoid a stall, but the seaplane responded more rapidly than he expected so he increased its pitch attitude to avoid a collision with the water. The seaplane ultimately climbed to about 30 feet above the water before the pilot initiated a descent for a landing. The pilot reported that he “could not control the landing” and that the seaplane collided with the water in a nose-low and right-wing-low attitude. The pilot reported that there were no mechanical anomalies with the seaplane during the accident flight. In addition, he noted that his overall lack of flight experience in the seaplane contributed to the accident. 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 Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Pitch control-Not attained/maintained - C
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- F Personnel issues-Experience/knowledge-Experience/qualifications-Total experience-Pilot - F
Verbatim from NTSB's published report. Source file
NTSB_2013_CEN13LA418.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…
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