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.
Douglas, WY
THE ACFT LOST ENGINE POWER ABOUT 400 FT AGL DURING INITIAL CLIMB AFTER TAKEOFF AND THE PILOT INITIATED AN EMERGENCY FORCED LANDING ON A PUBLIC ROAD. THE ACFT WING IMPACTED THE POST OF A NARROW CATTLE GUARD ACROSS THE ROAD DURING LANDING GROUND ROLL AND THE ACFT SLID OFF THE ROAD. THE ENGINE QUIT AGAIN WHILE IT WAS BEING TESTED AFTER THE ACCIDENT. AN EXAM OF THE ENGINE FUEL SYSTEM REVEALED THE ENGINE FUEL PUMP VAPOR RETURN JET WAS PLUGGED WITH A SMALL PIECE OF BLACK, CRESCENT SHAPED, RUBBER MATERIAL. A NEW FUEL HOSE TO THE ENGINE FUEL PUMP, MADE OF BLACK RUBBER MATERIAL, WAS INSTALLED AT THE LAST ANNUAL INSPECTION.
THE IMPROPER MAINTENANCE/REPLACEMENT OF A FUEL HOSE AND THE BLOCKED FUEL VAPOR RETURN SYSTEM. A FACTOR RELATING TO THE ACCIDENT WAS THE CATTLE GUARD FENCE POSTS BESIDE THE ROAD.
THE ACFT LOST ENGINE POWER ABOUT 400 FT AGL DURING INITIAL CLIMB AFTER TAKEOFF AND THE PILOT INITIATED AN EMERGENCY FORCED LANDING ON A PUBLIC ROAD. THE ACFT WING IMPACTED THE POST OF A NARROW CATTLE GUARD ACROSS THE ROAD DURING LANDING GROUND ROLL AND THE ACFT SLID OFF THE ROAD. THE ENGINE QUIT AGAIN WHILE IT WAS BEING TESTED AFTER THE ACCIDENT. AN EXAM OF THE ENGINE FUEL SYSTEM REVEALED THE ENGINE FUEL PUMP VAPOR RETURN JET WAS PLUGGED WITH A SMALL PIECE OF BLACK, CRESCENT SHAPED, RUBBER MATERIAL. A NEW FUEL HOSE TO THE ENGINE FUEL PUMP, MADE OF BLACK RUBBER MATERIAL, WAS INSTALLED AT THE LAST ANNUAL INSPECTION.