ANC14CA089
2014-09-29 · Kodiak, Alaska, United States · None · 1 aircraft · Status: Completed
Airport ADQ
Aircraft involved
Probable cause & findings
The pilots failure to maintain control of the airplane while taxiing in gusty wind conditions.
Factual narrative
The pilot was back taxiing on the runway for departure in a tundra tire tailwheel-equipped airplane. He stated he had made one takeoff from the airport earlier that day, he had checked the weather before this departure and noticed that the wind had increased slightly. There were other aircraft using the same runway and he felt confident that he could handle the wind. While back taxiing he noticed that he was using heavy braking when a gust of wind pushed the airplane to the left. He stated that the brakes were too hot to hold the aircraft straight, resulting in a ground loop. The airplane sustained substantial damage to the left and right wing, aileron, horizontal stabilizer, and elevator. The pilot stated that there were no preaccident mechanical anomalies with the airplane that would have precluded normal operation.The pilot stated in the recommendation section of the NTSB Accident/Incident Reporting Form 6120.1, that the large 29 inch tundra tires caused the brakes to heat up much faster than the 850 tires that he was used to. He recommended limiting downwind taxiing to short distances, and in no more than 12 knots of wind while operating with large tires. The pilot was back taxiing on the runway for departure in a tundra tire tailwheel-equipped airplane. He stated he had made one takeoff from the airport earlier that day, he had checked the weather before this departure and noticed that the wind had increased slightly. There were other aircraft using the same runway and he felt confident that he could handle the wind. While back taxiing he noticed that he was using heavy braking when a gust of wind pushed the airplane to the left. He stated that the brakes were too hot to hold the aircraft straight, resulting in a ground loop. The airplane sustained substantial damage to the left and right wing, aileron, horizontal stabilizer, and elevator. The pilot stated that there were no preaccident mechanical anomalies with the airplane that would have precluded normal operation.The pilot stated in the recommendation section of the NTSB Accident/Incident Reporting Form 6120.1, that the large 29 inch tundra tires caused the brakes to heat up much faster than the 850 tires that he was used to. He recommended limiting downwind taxiing to short distances, and in no more than 12 knots of wind while operating with large tires. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
FAA avdata. C = Cause, F = Factor.
- C Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot - C
- C Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Directional control-Not attained/maintained - C
- — Environmental issues-Conditions/weather/phenomena-Wind-Gusts-Effect on operation
Verbatim from NTSB's published report. Source file
NTSB_2014_ANC14CA089.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Search this event elsewhere
External sources are reported, not agency: signal that something happened, not fact about what happened.
- TallyAero Live Wire Aviation press
- NTSB CAROL Agency ↗
- NTSB Docket Agency ↗
- Aviation Safety Network Aviation press ↗
- Kathryn's Report Aviation press ↗
- Aviation Herald Aviation press ↗
- AVweb Aviation press ↗
- Pilots of America Community ↗
- Reddit /r/flying Community ↗
- FlightAware Aviation press ↗
- AOPA accident database Aviation press ↗
- Google News News ↗
- DuckDuckGo News ↗
Related research
Matched on aircraft type. All research papers
- arXiv 2026 · arXiv preprint A Miniaturized Broadband 1-Bit Coding Reconfigurable Intelligent Surface for NLOS UE Localization and Uplink Communication
In this paper, a broadband 1-bit coding metasurface-based reconfigurable intelligent surface (RIS) is presented. The unit cell of the metasurface consists of a wide dipole modified with interdigital c…
- arXiv 2024 · arXiv preprint Distilling Tiny and Ultra-fast Deep Neural Networks for Autonomous Navigation on Nano-UAVs
Nano-sized unmanned aerial vehicles (UAVs) are ideal candidates for flying Internet-of-Things smart sensors to collect information in narrow spaces.
- Embry-Riddle Scholarly Commons 2024 · Conference paper Integrated Propulsion and Control of Rotorcraft
RESEARCH OBJECTIVE OVERVIEW The Eagle Flight Research Center (EFRC) at Embry-Riddle Aeronautical University (ERAU) is investigating the handling qualities of failure modes of multi-rotors employing di…
- NASA NTRS 2023 · Presentation Subsonic Single Aft Engine (SUSAN) Flight Deck Experiment: Throttle and Engine Display Concepts
NASA is developing a new hybrid-electric aircraft concept called the SUbsonic Single Aft eNgine (SUSAN) Electrofan. The SUSAN airplane is being designed as a 180-passenger commercial regional jet and …
- Embry-Riddle Scholarly Commons 2023 · Conference paper The Value of Strong Partnerships to Build a Successful Aviation Maintenance Career Pathway Program for Transitioning Military Service Members
The aerospace industry is competing with other industries for a qualified workforce, and many of those competing industries are investing heavily in creating workforce development pipelines.
- FAA-affiliated R&D (MITRE / Volpe / FAA Tech Center) 2022 · FAA Tech Center report (DOT/FAA/TC-22/08) Lithium Battery Thermal Runaway in Aircraft Cargo Holds
Hughes Technical Center fire-research evaluation of lithium-ion battery thermal runaway in Class C cargo compartments. Drove revisions to FAR 25 cargo fire-suppression certification and the SAFO 18001…