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.
Englewood, CO
The prevailing wind favored landing on runway 28, but it was closed due to a previous incident and the airplane was blocking the runway. The pilot accepted runway 35R for landing. The wind was from 290 degrees at 20 knots, with gusts to 28 knots. As the pilot aligned the airplane with the runway, he noticed 'snow fingers' across the runway so he planned his touchdown between the centerline and the right side of the runway. The airplane touched down and the crosswind caused the airplane to drift right. The airplane was substantially damaged when it struck a snow berm on the right side of the runway. According to the Beech Aircraft Corporation, the maximum demonstrated crosswind component for the Beech 35-B33 is 17 knots. This would produce a crosswind component of about 17 knots and a headwind component about 10 knots. Gusts of 28 knots would produce a crosswind component of about 24 knots and a headwind component of 14 knots.
The pilot's improper decision to land in wind conditions that exceeded the airplane's crosswind component, and his failure to divert to an alternate airport with runways more nearly aligned with the wind. Factors were the icy runway and crosswind.
On December 27, 1997, at 1451 mountain standard time, a Beech 35-B33, N5743K, owned and operated by the pilot, was substantially damaged when it collided with a snow berm while landing at Englewood, Colorado. The private pilot and his passenger sustained minor injuries. Visual meteorological conditions prevailed, and no flight plan was filed for the personal flight conducted under Title 14 CFR Part 91. The flight originated at Fort Worth, Texas, at 1115 central standard time, and made an en route stop at Wichita Falls, Texas. According to the pilot, the prevailing wind favored landing on runway 28. The runway, however, was closed due to a previous incident and the airplane was blocking the runway. The pilot accepted runway 35R for landing. He said control tower personnel told him the wind was from 290 degrees at 20 knots, with gusts to 28 knots. As the pilot aligned the airplane with the runway, he noticed "snow fingers" across the runway so he planned his touchdown between the centerline and the right side of the runway. The airplane touched down and the crosswind caused the airplane to drift right. The airplane struck a snow berm on the right side of the runway, causing it to spin around. According to the Beech Aircraft Corporation, the maximum demonstrated crosswind component for the Beech 35-B33 is 17 knots. Plotting the reported wind on the wind component chart, it was determined that a 60 degree crosswind at 20 knots would produce a crosswind component of about 17 knots and a headwind component about 10 knots. Gusts of 28 knots would produce a crosswind component of about 24 knots and a headwind component of 14 knots. There was substantial damage to the right wing. Additionally, the landing gear collapsed and the engine was torn loose from its mounts.