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.
Romeo, MI
THE PILOTS STATED THAT THE EN ROUTE FLIGHT AND APPROACH TO LANDING WERE ROUTINE. AFTER TOUCHDOWN, AS THE AIRCRAFT SETTLED TO THE GROUND, THE LEFT WING DROPPED AND THE AIRCRAFT VEERED OFF THE LEFT SIDE OF THE RUNWAY. POST-ACCIDENT EXAMINATION REVEALED THAT THE LEFT MAIN LANDING GEAR ASSEMBLY HAD FAILED DUE TO STRESS CORROSION. THE AIRCRAFT HAD 495 HOURS TOTAL TIME, WITH 45 HOURS SINCE THE MOST RECENT ANNUAL INSPECTION, WHICH OCCURRED IN JUNE 1988.
THE FAILURE OF THE LEFT MAIN LANDING GEAR ASSEMBLY DUE TO STRESS CORROSION.
THE PILOTS STATED THAT THE EN ROUTE FLIGHT AND APPROACH TO LANDING WERE ROUTINE. AFTER TOUCHDOWN, AS THE AIRCRAFT SETTLED TO THE GROUND, THE LEFT WING DROPPED AND THE AIRCRAFT VEERED OFF THE LEFT SIDE OF THE RUNWAY. POST-ACCIDENT EXAMINATION REVEALED THAT THE LEFT MAIN LANDING GEAR ASSEMBLY HAD FAILED DUE TO STRESS CORROSION. THE AIRCRAFT HAD 495 HOURS TOTAL TIME, WITH 45 HOURS SINCE THE MOST RECENT ANNUAL INSPECTION, WHICH OCCURRED IN JUNE 1988.