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.
Fayetteville, NC
THE PILOT REPORTED A FUEL PUMP PROBLEM TO FAYETTEVILLE TOWER AND REQUESTED LANDING. THE PILOT WAS CLEARED TO LAND ON RUNWAY 04. THE CONTROLLER NOTICED THAT THE PILOT HAD NOT LOWERED THE LANDING GEAR. THE PILOT WAS QUESTIONED CONCERNING THE GEAR. INSTEAD OF CONTINUING THE APPROACH THE PILOT TURNED WEST AND WAS OBSERVED CIRCLING, THEN FALLING BELOW THE TREE LINE. THE WRECKAGE SITE EXAMINATION DISCLOSED THAT THE AIRPLANE CRASHED IN NOSE LOW ATTITUDE ALONG A TREE LINE SOUTH OF AN OPEN FIELD. THE EXAMINATION ALSO DISCLOSED THAT THE FUEL PUMPS ON THE LEFT ENGINE HAD FAILED. THE ENGINE DRIVEN PUMP HAD A SHAFT FAILURE. THE BOOST PUMP HAD AN INTERNAL SHORT. THE LEFT PROPELLER WAS IN THE FEATHER POSITION. THE OPEN FIELD HAD AMPLE SPACE FOR AN EMERGENCY LANDING. THE RIGHT ENGINE WAS STILL CAPABLE OF OPERATION.
THE PILOT REPORTED A FUEL PUMP PROBLEM TO FAYETTEVILLE TOWER AND REQUESTED LANDING. THE PILOT WAS CLEARED TO LAND ON RUNWAY 04. THE CONTROLLER NOTICED THAT THE PILOT HAD NOT LOWERED THE LANDING GEAR. THE PILOT WAS QUESTIONED CONCERNING THE GEAR. INSTEAD OF CONTINUING THE APPROACH THE PILOT TURNED WEST AND WAS OBSERVED CIRCLING, THEN FALLING BELOW THE TREE LINE. THE WRECKAGE SITE EXAMINATION DISCLOSED THAT THE AIRPLANE CRASHED IN NOSE LOW ATTITUDE ALONG A TREE LINE SOUTH OF AN OPEN FIELD. THE EXAMINATION ALSO DISCLOSED THAT THE FUEL PUMPS ON THE LEFT ENGINE HAD FAILED. THE ENGINE DRIVEN PUMP HAD A SHAFT FAILURE. THE BOOST PUMP HAD AN INTERNAL SHORT. THE LEFT PROPELLER WAS IN THE FEATHER POSITION. THE OPEN FIELD HAD AMPLE SPACE FOR AN EMERGENCY LANDING. THE RIGHT ENGINE WAS STILL CAPABLE OF OPERATION.