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.
Howard, WI
THE ACCIDENT AIRPLANE LOST ENGINE POWER DURING INITIAL CLIMB FROM A PRIVATE LANDING STRIP. THE AIRPLANE LANDED ON A HIGHWAY AND COLLIDED WITH A SIGN DURING THE LANDING ROLL. THE PILOT TOLD INSPECTORS FROM THE FEDERAL AVIATION ADMINISTRATION (FAA) THAT THE ENGINE HAD STARTED MISSING DURING TAKEOFF AND THEN STOPPED COMPLETELY APPROXIMATELY 300 FEET ABOVE THE GROUND. HE TOLD THEM HE SWITCHED FUEL TANKS AND ATTEMPTED A RESTART BUT WAS UNSUCCESSFUL. FAA INSPECTORS EXAMINED THE AIRPLANE AFTER THE ACCIDENT. THEY VERIFIED MECHANICAL CONTINUITY THROUGHOUT THE FLIGHT CONTROL SYSTEM. THERE WERE NO DEFECTS DISCOVERED IN THE ENGINE. EXAMINATION OF THE FUEL SYSTEM SHOWED SEDIMENT AND FOREIGN MATERIAL IN THE GASCOLATOR BOWL.
AN INADEQUATE PREFLIGHT INSPECTION BY THE PILOT IN COMMAND AND A LOSS OF ENGINE POWER FROM CONTAMINATED FUEL.
THE ACCIDENT AIRPLANE LOST ENGINE POWER DURING INITIAL CLIMB FROM A PRIVATE LANDING STRIP. THE AIRPLANE LANDED ON A HIGHWAY AND COLLIDED WITH A SIGN DURING THE LANDING ROLL. THE PILOT TOLD INSPECTORS FROM THE FEDERAL AVIATION ADMINISTRATION (FAA) THAT THE ENGINE HAD STARTED MISSING DURING TAKEOFF AND THEN STOPPED COMPLETELY APPROXIMATELY 300 FEET ABOVE THE GROUND. HE TOLD THEM HE SWITCHED FUEL TANKS AND ATTEMPTED A RESTART BUT WAS UNSUCCESSFUL. FAA INSPECTORS EXAMINED THE AIRPLANE AFTER THE ACCIDENT. THEY VERIFIED MECHANICAL CONTINUITY THROUGHOUT THE FLIGHT CONTROL SYSTEM. THERE WERE NO DEFECTS DISCOVERED IN THE ENGINE. EXAMINATION OF THE FUEL SYSTEM SHOWED SEDIMENT AND FOREIGN MATERIAL IN THE GASCOLATOR BOWL.