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.
Toledo, WA
THE PILOT REPORTED THAT BEFORE LANDING, HE TURNED THE FUEL BOOST "ON", APPLIED CARBURETOR HEAT, AND SET THE POWER AT ROUGHLY 1500 RPM. HE REPORTED THAT THE MIXTURE HAD BEEN IN THE FULL RICH POSITION DURING THE ENTIRE FLIGHT. HE ENCOUNTERED A CROSSWIND ON FINAL APPROACH AND ATTEMPTED A POWER CORRECTION. HOWEVER, THERE WAS NO ENGINE RESPONSE. SUBSEQUENTLY, THE AIRCRAFT WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING OFF OF THE AIRPORT. NO RESTART WAS ATTEMPTED. AN INVESTIGATION REVEALED NO PRECRASH MALFUNCTION OR FAILURE OF THE AIRCRAFT OR ENGINE. HOWEVER, IT WAS NOTED THAT THE MAJORITY OF THE PILOT'S FLIGHT EXPERIENCE WAS IN A CESSNA 172. ALSO, IT WAS NOTED THAT THE MIXTURE CONTROL IN PIPER PA-28, N9544J, WAS SIMILAR TO THE CARBURETOR HEAT CONTROL IN MANY CESSNA 172 AIRCRAFT.
THE PILOT REPORTED THAT BEFORE LANDING, HE TURNED THE FUEL BOOST "ON", APPLIED CARBURETOR HEAT, AND SET THE POWER AT ROUGHLY 1500 RPM. HE REPORTED THAT THE MIXTURE HAD BEEN IN THE FULL RICH POSITION DURING THE ENTIRE FLIGHT. HE ENCOUNTERED A CROSSWIND ON FINAL APPROACH AND ATTEMPTED A POWER CORRECTION. HOWEVER, THERE WAS NO ENGINE RESPONSE. SUBSEQUENTLY, THE AIRCRAFT WAS SUBSTANTIALLY DAMAGED DURING A FORCED LANDING OFF OF THE AIRPORT. NO RESTART WAS ATTEMPTED. AN INVESTIGATION REVEALED NO PRECRASH MALFUNCTION OR FAILURE OF THE AIRCRAFT OR ENGINE. HOWEVER, IT WAS NOTED THAT THE MAJORITY OF THE PILOT'S FLIGHT EXPERIENCE WAS IN A CESSNA 172. ALSO, IT WAS NOTED THAT THE MIXTURE CONTROL IN PIPER PA-28, N9544J, WAS SIMILAR TO THE CARBURETOR HEAT CONTROL IN MANY CESSNA 172 AIRCRAFT.