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.
Roanoke, TX
During initial climb, the airplane's single engine experienced a partial loss of power. Unable to maintain altitude, the pilot performed an emergency landing to a field. During the landing rollout, the airplane impacted a rock and the nose landing gear collapsed, damaging the firewall. The airplane came to rest in a nose-down position and the pilot was able to exit unassisted. Following the accident, an examination of the airplane revealed that the throttle control rod-end to carburetor throttle arm hardware was missing. In addition, the airplane had not been inspected in accordance with an annual inspection during the previous year.
The partial loss of engine power due to a failure of the throttle control rod-end to carburetor arm hardware. A contributing factor was the pilot's decision to fly the airplane without a current annual inspection.
During initial climb, the airplane's single engine experienced a partial loss of power. Unable to maintain altitude the pilot performed an emergency landing to a field. During the landing rollout, the airplane impacted a rock and the nose landing gear collapsed. The airplane came to rest in a nose down position and the pilot was able to exit unassisted. Following the accident, an examination of the airplane revealed that the firewall had sustained structural damage, and the throttle control rod-end to carburetor throttle arm hardware was missing. In addition, the airplane had not been inspected in accordance with an annual inspection during the previous year.