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.
Clarksdale, MS
THE PILOT REPORTED NO INDICATION OF ENGINE MALFUNCTION DURING TAKEOFF AND CLIMB-OUT. HOWEVER, AFTER TURNING IN A DOWNWIND DIRECTION, HE NOTED A LOSS OF AIRSPEED AND POWER. HE STATED THAT THE POWER LOSS WAS SO GRADUAL THAT HE NOTICED NOTHING UNUSUAL UNTIL THE PLANE BEGAN LOSING AIRSPEED. HE TURNED AWAY FROM A WOODED AREA AND SWAMP GROUND. ALSO, HE TRIED TO DUMP THE DRY FERTILIZER, BUT REPORTED THAT THE MATERIAL APPARENTLY CHOKED UP IN THE SPREADER THROAT AND WOULD NOT DUMP. THE PILOT WAS FORCED TO LAND WITH A TAILWIND IN A MUDDY, CULTIVATED FIELD TO AVOID TREES AND HIGHLINE WIRES. DURING LANDING, THE PLANE NOSED OVER. AN INVESTIGATION REVEALED THAT THE NUMBER 4 CYLINDER FUEL INJECTOR NOZZLE LINE HAD SEPARATED NEAR THE FERRULE AT THE NOZZLE END. THE LINE FAILED FROM FATIGUE.
THE PILOT REPORTED NO INDICATION OF ENGINE MALFUNCTION DURING TAKEOFF AND CLIMB-OUT. HOWEVER, AFTER TURNING IN A DOWNWIND DIRECTION, HE NOTED A LOSS OF AIRSPEED AND POWER. HE STATED THAT THE POWER LOSS WAS SO GRADUAL THAT HE NOTICED NOTHING UNUSUAL UNTIL THE PLANE BEGAN LOSING AIRSPEED. HE TURNED AWAY FROM A WOODED AREA AND SWAMP GROUND. ALSO, HE TRIED TO DUMP THE DRY FERTILIZER, BUT REPORTED THAT THE MATERIAL APPARENTLY CHOKED UP IN THE SPREADER THROAT AND WOULD NOT DUMP. THE PILOT WAS FORCED TO LAND WITH A TAILWIND IN A MUDDY, CULTIVATED FIELD TO AVOID TREES AND HIGHLINE WIRES. DURING LANDING, THE PLANE NOSED OVER. AN INVESTIGATION REVEALED THAT THE NUMBER 4 CYLINDER FUEL INJECTOR NOZZLE LINE HAD SEPARATED NEAR THE FERRULE AT THE NOZZLE END. THE LINE FAILED FROM FATIGUE.