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.
Inverness, FL
DURING CRUISE FLT A TOTAL LOSS OF ENGINE POWER WAS EXPERIENCED. THE PLT WAS ATTEMPTING A FORCED LANDING WHEN THE ACFT CONTACTED ELECTRICAL WIRES AND A TREE PRIOR TO COLLIDING WITH THE TERRAIN. POST ACCIDENT INSPECTION REVEALED THE PROPELLER GOVERNOR OIL LINE CRACKED TO THE POINT THAT ENGINE OIL PUMPED OUT OF THE ENGINE WHICH SUBSEQUENTLY SEIZED. THE OIL LINE WAS INSTALLED AFTER ENGINE OVERHAUL WITHOUT TWO CLAMPS AND WAS BENT IN THE AREA WHERE THE ALTERNATOR BELT IS ADJUSTED. THE BENDING DAMAGE CAUSED A FATIGUE CRACK IN THE LINE AND THE LACK OF SUPPORT CLAMPS AIDED IN THE CRACKING PROCESS.
THE FAILURE OF THE PROPELLER GOVERNOR OIL LINE DUE TO FATIGUE WHICH WAS CAUSED BY BENDING DAMAGE TO THE LINE AND THE FAILURE OF MECHANICS TO INSTALL SUPPORT CLAMPS ON THE LINE WHICH CAUSED THE FATIGUE TO PROPAGATE AT A FASTER RATE.
DURING CRUISE FLT A TOTAL LOSS OF ENGINE POWER WAS EXPERIENCED. THE PLT WAS ATTEMPTING A FORCED LANDING WHEN THE ACFT CONTACTED ELECTRICAL WIRES AND A TREE PRIOR TO COLLIDING WITH THE TERRAIN. POST ACCIDENT INSPECTION REVEALED THE PROPELLER GOVERNOR OIL LINE CRACKED TO THE POINT THAT ENGINE OIL PUMPED OUT OF THE ENGINE WHICH SUBSEQUENTLY SEIZED. THE OIL LINE WAS INSTALLED AFTER ENGINE OVERHAUL WITHOUT TWO CLAMPS AND WAS BENT IN THE AREA WHERE THE ALTERNATOR BELT IS ADJUSTED. THE BENDING DAMAGE CAUSED A FATIGUE CRACK IN THE LINE AND THE LACK OF SUPPORT CLAMPS AIDED IN THE CRACKING PROCESS.