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.
Carlisle, AR
THE AG PILOT, WITH AN EMPTY AIRPLANE, ON TAKEOFF ON A SHORT STRIP, SAW THE TACHOMETER OVERSPEED. HE ABORTED THE TAKEOFF BUT WAS UNABLE TO STOP ON THE ROUGH/UNEVEN SURFACE. HE SAID THAT WHEN THE END OF THE RUNWAY GOT CLOSER, THE SURFACE GOT BETTER, AND HE APPLIED FULL BRAKING ACTION, AND THE AIRPLANE FLIPPED FORWARD TO THE INVERTED POSITION. THE OWNER PUT THE TACHOMETER IN ANOTHER AIRPLANE AND IT OPERATED NORMALLY. OPERATOR OF ENGINE OVERHAUL SHOP CONTACTED MANUFACTURER FOR SPECIAL INSTRUCTIONS FOR INSPECTING FOR ENGINE OVERSPEED. MANUFACTURER REPLIED THAT ENGINE OVERSPEED NOT POSSIBLE WITH THIS ENGINE/PROPELLER COMBINATION DUE TO INTERNAL CONSTRUCTION OF PROPELLER.
PILOT'S INITIATION OF THE ABORT WITH EXCESS AIRSPEED. A CONTRIBUTING FACTOR WAS THE ENGINE TACHOMETER OVERSPEED.
THE AG PILOT, WITH AN EMPTY AIRPLANE, ON TAKEOFF ON A SHORT STRIP, SAW THE TACHOMETER OVERSPEED. HE ABORTED THE TAKEOFF BUT WAS UNABLE TO STOP ON THE ROUGH/UNEVEN SURFACE. HE SAID THAT WHEN THE END OF THE RUNWAY GOT CLOSER, THE SURFACE GOT BETTER, AND HE APPLIED FULL BRAKING ACTION, AND THE AIRPLANE FLIPPED FORWARD TO THE INVERTED POSITION. THE OWNER PUT THE TACHOMETER IN ANOTHER AIRPLANE AND IT OPERATED NORMALLY. OPERATOR OF ENGINE OVERHAUL SHOP CONTACTED MANUFACTURER FOR SPECIAL INSTRUCTIONS FOR INSPECTING FOR ENGINE OVERSPEED. MANUFACTURER REPLIED THAT ENGINE OVERSPEED NOT POSSIBLE WITH THIS ENGINE/PROPELLER COMBINATION DUE TO INTERNAL CONSTRUCTION OF PROPELLER.