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.
Redwood, MS
THE ACFT MADE A FORCED LANDING IN A SOYBEAN FIELD AFTER SEVERE VIBRATION DEVELOPED DURING A SPRAYING OPERATION. THE PILOT STATED THAT THE POWERPLANT AND FLT CONTROLS WERE FUNCTIONING NORMALLY AT THE TIME OF THE ACCIDENT. AN ON-SCENE INVESTIGATION REVEALED THAT THE COUNTERWEIGHT BEARING SHAFT (P/N 63546) BROKE ALLOWING THE PROPELLER BLADE TO GO TO HIGHER PITCH WHILE THE OTHER BLADE REMAINED AT CRUISE PITCH SETTING. EXAMINATION OF BOTH PROPELLER BLADE COUNTERWEIGHTS REVEALED THAT THE INTERNAL PARTS HAD MINIMUM AMOUNT OF LUBRICATION. THE SHAFT THAT BROKE WAS ALSO RUSTY AND THE INNER BEARING RACE WAS BROKEN WITH 5 BALL BEARING MISSING. THERE WERE OTHER MAINTENANCE DICREPANCIES ON THIS SHAFT ASSEMBLY. THE TOTAL TIME OF THIS HAMILTON STANDARD 12D40 PROPELLER IS UNKNOWN. THE TIME SINCE THE ACFT WAS INSPECTED IS 194 HOURS.
THE ACFT MADE A FORCED LANDING IN A SOYBEAN FIELD AFTER SEVERE VIBRATION DEVELOPED DURING A SPRAYING OPERATION. THE PILOT STATED THAT THE POWERPLANT AND FLT CONTROLS WERE FUNCTIONING NORMALLY AT THE TIME OF THE ACCIDENT. AN ON-SCENE INVESTIGATION REVEALED THAT THE COUNTERWEIGHT BEARING SHAFT (P/N 63546) BROKE ALLOWING THE PROPELLER BLADE TO GO TO HIGHER PITCH WHILE THE OTHER BLADE REMAINED AT CRUISE PITCH SETTING. EXAMINATION OF BOTH PROPELLER BLADE COUNTERWEIGHTS REVEALED THAT THE INTERNAL PARTS HAD MINIMUM AMOUNT OF LUBRICATION. THE SHAFT THAT BROKE WAS ALSO RUSTY AND THE INNER BEARING RACE WAS BROKEN WITH 5 BALL BEARING MISSING. THERE WERE OTHER MAINTENANCE DICREPANCIES ON THIS SHAFT ASSEMBLY. THE TOTAL TIME OF THIS HAMILTON STANDARD 12D40 PROPELLER IS UNKNOWN. THE TIME SINCE THE ACFT WAS INSPECTED IS 194 HOURS.