NTSB CAROL · Event
Event SEA05LA042
Aircraft involved
Probable cause & findings
The pilot's improper flare. Factors contributing to the accident included the pilot's improper approach and the glassy water condition.
Factual narrative
On February 3, 2005, approximately 1000 Pacific standard time, a single-engine Maule M-7-260 amphibian airplane, N977BE, was substantially damaged while attempting to land on Lake Sutherland, located 10 nautical miles west-southwest of Port Angeles, Washington. The certificated commercial pilot and his sole passenger were not injured. Visual meteorological conditions prevailed for the personal flight, which was conducted in accordance with 14 CFR Part 91, and a flight plan was not filed. The flight departed the Diamond Point Airstrip, Sequim, Washington, at 0930, with the destination being Lake Sutherland. In a written statement provided to the NTSB investigator-in-charge, the pilot reported that upon arriving over Lake Sutherland the planned approach was to land on the western half of the lake. The pilot stated there was no traffic, no obstructions, the wind was calm, and that "glassy water" conditions existed. The pilot further stated that he proceeded westerly on a left downwind leg to the lake and made a "U-shaped" turn to final just west of the shoreline, with his final approach being on an easterly heading. The pilot related that as he crossed the shoreline he decreased power to increase the descent rate, and utilizing visual cues he was about to add power to level off when the airplane impacted the water. The pilot and his passenger exited the airplane unassisted and without injury. In a written statement the passenger reported, "...the approach appeared normal until we entered a position where the surface of the water could not be distinguished from sky. Approximately two seconds later after reaching this point we impacted the water." The pilot reported that the airplane sustained structural and water damage to the entire aircraft, with the exception of possibly the empennage and tail section. According to Federal Aviation Publication FAA-H-8083-23, "Seaplane, Skiplane, and Float/Ski Equipped Helicopter Operations Handbook," Chapter 6 - Seaplane Operations, Glassy Water Landing, the proper procedure for conducting a glassy water landing is to, "Always perform glassy water landings with power. Perform a normal approach, but prepare as though intending to land at an altitude well above the surface. This altitude might be 200 feet above the surface. The objective is to have the seaplane ready to contact the water soon after if reaches the target altitude, so at approximately 200 feet above the surface, raise the nose to the altitude normally used for touchdown, and adjust the power to provide a constant descent rate of no more than 150 feet per minute at an airpseed approximately 10 knots above stall speed. Maintain this attitude, airspeed, and rate of descent until the seaplane contacts the water." The wind was calm and glassy water conditions prevailed as the pilot approached from the east, intending to land on the western half of the lake. Using visual cues and reducing power to increase his rate of descent, the pilot's delayed landing flare resulted in the airplane impacting the water in a nose low attitude. The entire aircraft sustained structural and water damage, with the exception of the empennage and tail section. Source: NTSB Aviation Accident Database (Pre-2008 Archive) Retrieved: 2026-02-12
Verbatim from NTSB's published report. Source file
NTSB_2005_SEA05LA042.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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