NTSB CAROL · Event
Event ANC14CA061
Aircraft involved
Probable cause & findings
The pilot's decision to takeoff from a remote mountain lake in variable wind. Contributing to the accident was the pilots delayed decision to abort the takeoff.
Factual narrative
The pilot was departing from a remote mountain lake in an amphibious float-equipped airplane. Prior to departure he observed the wind out of the east, and began his takeoff run in an easterly direction. He stated that the airplane was slow to accelerate and unstable once on the step. He closed the throttle and aborted the takeoff, the airplane immediately yawed to the right, he applied left rudder and deployed the water rudders in an effort to correct for the yaw, but the right wing impacted a tree and swung the airplane into the shoreline. The airplane sustained substantial damage to the right wing and right lift strut. The pilot stated that there were no preaccident mechanical anomalies with the airplane that would have precluded normal operation. While awaiting rescue, the pilot noted that the wind reversed direction about the center of the lake, and he may have encountered a tailwind during the takeoff run. In the recommendation section of the NTSB Accident/Incident Reporting Form 6120.1, the pilot stated that the accident may have been avoided if he had made the decision to abort the takeoff sooner. The pilot was departing from a remote mountain lake in an amphibious float-equipped airplane. Prior to departure he observed the wind out of the east, and began his takeoff run in an easterly direction. He stated that the airplane was slow to accelerate and unstable once on the step. He closed the throttle and aborted the takeoff, the airplane immediately yawed to the right, he applied left rudder and deployed the water rudders in an effort to correct for the yaw, but the right wing impacted a tree and swung the airplane into the shoreline. The airplane sustained substantial damage to the right wing and right lift strut. The pilot stated that there were no preaccident mechanical anomalies with the airplane that would have precluded normal operation. While awaiting rescue, the pilot noted that the wind reversed direction about the center of the lake, and he may have encountered a tailwind during the takeoff run. In the recommendation section of the NTSB Accident/Incident Reporting Form 6120.1, the pilot stated that the accident may have been avoided if he had made the decision to abort the takeoff sooner. 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-Info processing/decision-Decision making/judgment-Pilot - C
- C Environmental issues-Conditions/weather/phenomena-Wind-Variable wind-Decision related to condition - C
- F Personnel issues-Action/decision-Action-Delayed action-Pilot - F
Verbatim from NTSB's published report. Source file
NTSB_2014_ANC14CA061.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. 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 2019 · Conference Paper
Crash Testing and Simulation of a Cessna 172 Aircraft: Pitch Down Impact Onto Soft Soil
During the summer of 2015, NASA Langley Research Center conducted three full-scale crash tests of Cessna 172 (C-172) aircraft at the NASA Langley Landing and Impact Research (LandIR) Facility.
- NASA NTRS 2019 · Technical Memorandum (TM)
Simulating the Impact Response of Three Full-Scale Crash Tests of Cessna 172 Aircraft
During the summer of 2015, a series of three full-scale crash tests were performed at the Landing and Impact Research Facility located at NASA Langley Research Center of Cessna 172 aircraft.
- NASA NTRS 2019 · Other - NACA Research Memorandum
Ditching Tests of a 1/18-Scale Model of the Lockheed Constellation Airplane
Tests were made of a 1/18-scale dynamically similar model of the Lockheed Constellation airplane to investigate its ditching characteristics and proper ditching technique.
- NASA NTRS 2019 · Other - NACA Research Memorandum
Ditching Tests with a 1/12-Scale Model of the Army A-26 Airplane in Langley Tank No. 2 and on an Outdoor Catapult
Tests were conducted in calm water in Langley tank no. 2 and in calm and rough water at an outdoor catapult in order to determine the best way to make a forced landing of an Army A-26 airplane and to …
- NASA NTRS 2019 · Other - NACA Research Memorandum
Ditching Investigation of a 1/15-Scale Model of the Convair-Liner Airplane
A ditching investigation of a model of the Convair-Liner airplane was made to observe the behavior and determine the safest procedure for making an emergency water landing.
- NASA NTRS 2019 · Other - NACA Research Memorandum
Ditching Tests of a 1/18-Scale Model of the Lockheed Constellation Airplane with Speedpak Attached
Results of previous model ditching tests of the Lockheed Constellation airplane are reported. Further model tests have been made to determine the probable ditching characteristics and the proper ditch…
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