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.
Bainbridge, GA
WHILE EN ROUTE, THE PLT NOTED A SEVERE ENG VIBRATION. HE SHUT DOWN THE ENG & MADE AN EMERGENCY LANDING. DURING THE ROLL-OUT, THE ACFT HIT A DITCH & WAS DAMAGED. AN INVESTIGATION REVEALED THAT ONE PROP BLADE HAD FAILED FROM FATIGUE & THE END OF THE BLADE HAD SEPARATED. THE FATIGUE HAD ORIGINATED ON THE SIDE OF THE BLADE. THERE WERE INDICATIONS OF CORROSION WERE THE CRACK BEGAN, APRX 17' FROM THE BASE OF THE BLADE.
WHILE EN ROUTE, THE PLT NOTED A SEVERE ENG VIBRATION. HE SHUT DOWN THE ENG & MADE AN EMERGENCY LANDING. DURING THE ROLL-OUT, THE ACFT HIT A DITCH & WAS DAMAGED. AN INVESTIGATION REVEALED THAT ONE PROP BLADE HAD FAILED FROM FATIGUE & THE END OF THE BLADE HAD SEPARATED. THE FATIGUE HAD ORIGINATED ON THE SIDE OF THE BLADE. THERE WERE INDICATIONS OF CORROSION WERE THE CRACK BEGAN, APRX 17' FROM THE BASE OF THE BLADE.