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.
Kingston, NH
DURING FLIGHT, THE PILOT NOTICED THE ENGINE RPM WAS HIGH. HE WAS UNABLE TO CONTROL THE RPM WITH THE PROP CONTROL. HE REDUCED THE THROTTLE SETTING, BUT SOON THEREAFTER, THE ENGINE BEGAN RUNNING ROUGH WITH A SEVERE VIBRATION. THE PILOT SELECTED A FIELD FOR AN EMERGENCY LANDING, BUT WAS UNABLE TO REACH IT. SUBSEQUENTLY, THE AIRCRAFT IMPACTED AT THE TOP OF AN EMBANKMENT AND WAS EXTENSIVELY DAMAGED. DURING THE INVESTIGATION, FRESH OIL WAS FOUND ON THE EXTERIOR BOTTOM OF THE FUSELAGE FROM THE AREA OF THE FIREWALL TO THE TAIL. THE OIL PRESSURE INDICATOR HOSE WAS FOUND TO HAVE BEEN BROKEN OFF AT THE FIRE WALL (ON THE ENGINE SIDE). ALSO, A LARGE HOLE WAS FOUND IN THE CRANKCASE WHERE THE #2 CONNECTING ROD HAD FAILED.
DURING FLIGHT, THE PILOT NOTICED THE ENGINE RPM WAS HIGH. HE WAS UNABLE TO CONTROL THE RPM WITH THE PROP CONTROL. HE REDUCED THE THROTTLE SETTING, BUT SOON THEREAFTER, THE ENGINE BEGAN RUNNING ROUGH WITH A SEVERE VIBRATION. THE PILOT SELECTED A FIELD FOR AN EMERGENCY LANDING, BUT WAS UNABLE TO REACH IT. SUBSEQUENTLY, THE AIRCRAFT IMPACTED AT THE TOP OF AN EMBANKMENT AND WAS EXTENSIVELY DAMAGED. DURING THE INVESTIGATION, FRESH OIL WAS FOUND ON THE EXTERIOR BOTTOM OF THE FUSELAGE FROM THE AREA OF THE FIREWALL TO THE TAIL. THE OIL PRESSURE INDICATOR HOSE WAS FOUND TO HAVE BEEN BROKEN OFF AT THE FIRE WALL (ON THE ENGINE SIDE). ALSO, A LARGE HOLE WAS FOUND IN THE CRANKCASE WHERE THE #2 CONNECTING ROD HAD FAILED.