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.
Ada, MN
THE PILOT SPRAYED ONE FIELD AND PROCEEDED TO THE NEXT FIELD ABOUT 2 MILES AWAY. HE STATED THAT HE EXECUTED A TIGHT 270 DEG TURN TO THE RIGHT AT ABOUT 100 FT. HE ALSO STATED THAT AFTER ABOUT 90 DEG THROUGH THE TURN, THE AIRCRAFT LOST POWER, STALLED AND CRASHED. DURING AN INVESTIGATION, THE MAIN FUEL CONTROL VALVE WAS FOUND TO BE ABOUT 75% CLOSED. THE CABLE ASSEMBLY, PN 65227-06, THAT CONNECTS THE CONTROL KNOB IN THE COCKPIT TO THE MAIN FUEL CONTROL VALVE WAS DISCONNECTED FROM THE FUEL CONTROL VALVE BRACKET, PN 64304-00.
THE PILOT SPRAYED ONE FIELD AND PROCEEDED TO THE NEXT FIELD ABOUT 2 MILES AWAY. HE STATED THAT HE EXECUTED A TIGHT 270 DEG TURN TO THE RIGHT AT ABOUT 100 FT. HE ALSO STATED THAT AFTER ABOUT 90 DEG THROUGH THE TURN, THE AIRCRAFT LOST POWER, STALLED AND CRASHED. DURING AN INVESTIGATION, THE MAIN FUEL CONTROL VALVE WAS FOUND TO BE ABOUT 75% CLOSED. THE CABLE ASSEMBLY, PN 65227-06, THAT CONNECTS THE CONTROL KNOB IN THE COCKPIT TO THE MAIN FUEL CONTROL VALVE WAS DISCONNECTED FROM THE FUEL CONTROL VALVE BRACKET, PN 64304-00.