Overall Trends
Total, fatal, and serious accidents in the selected range.
Search investigations, review source evidence, monitor watched reports, and trace long-term patterns from one calm, data-first workspace.
Fast key and full-text search with live filters, watches, and precise metadata.
Use quotes for exact phrase matches (for example "fuel selector valve").
Track fatal and non-fatal accident patterns across Part 91, Part 135, and Part 121 operations.
Major cases, deep-report coverage, and investigation media across decades of NTSB history.
Move quickly by aircraft, airport, operator, and time with indexes built for research, not wandering.
NTSB Reports is an independent research and search tool for public aviation accident and incident records. It brings NTSB aviation reports, structured fields, docket files, extracted figures, photos, videos, and update history into one searchable interface.
The goal is practical safety education: make it faster to find relevant investigations, compare similar events, review factual records, and understand the evidence behind probable-cause and preliminary reports.
The investigative work and source records belong to the National Transportation Safety Board and the published investigation record. This site is not affiliated with or endorsed by the NTSB.
Dutch Harbor, AK
The airline transport pilot departed on a visual flight rules cross-country flight in a twin-engine airplane with two passengers aboard. He reported that during the flight the weather began changing and he arrived at the destination airport in unforecast deteriorating weather conditions. Unable to circle to land into the wind, the pilot elected to land on runway 12 with a gusting quartering right tailwind. During the landing roll, a wind gust pushed the nose of the airplane to the right, and the airplane began to slide momentarily on an icy patch on the runway. While sliding sideways, the left main landing gear contacted bare pavement, which resulted in the collapse of the left main landing gear. As a result, the airplane sustained substantial damage to the left wing. The wind at the airport before landing was reported to be out of 339 degrees at 26 knots, with gusts to 35 knots. According to the pilot operating handbook for the accident airplane, the maximum demonstrated crosswind component for the airplane is 20 knots, and a plot of the current wind conditions at the time of the accident showed that the crosswind component for the accident landing was 30 knots, 10 knots above the maximum demonstrated component. No preaccident mechanical anomalies that would have precluded normal operation were reported.
The pilot's decision to land in wind conditions that exceeded the airplane's demonstrated crosswind capability, which resulted in a loss of airplane control during the landing roll.
The airline transport pilot departed on a visual flight rules cross-country flight, in a twin-engine airplane, with two passengers aboard. During the flight, he reported that the weather began changing, and he arrived at the destination airport in deteriorating weather conditions. Unable to circle to land into the wind, he elected to land on runway 12 in gusting wind conditions, requiring a correction for a quartering right tailwind. During the landing roll, a wind gust pushed the nose of the airplane to the right, and the airplane began to slide momentary on an icy patch on the runway. While sliding sideways, the left main landing gear then contacted bare pavement, which loaded the left main landing gear strut, resulting in the collapse of the left main landing gear. As a result, the airplane sustained substantial damage to the left wing. Winds at the airport prior to landing were reported as 339 degrees magnetic at 26 knots, with gusts to 35 knots. According to the pilot operating handbook for the accident airplane, the maximum demonstrated crosswind component for the airplane is 20 knots, and a plot of the current wind conditions at the time of the accident showed that the crosswind component for the accident landing was 30 knots, 10 knots above the maximum demonstrated component. No preaccident mechanical anomalies were reported.