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.
Chesterfield, MO
THE ACFT CRASHED SHORT OF THE RWY AFTER MAKING A 180 DEG TURN AFTER TAKEOFF FOLLOWING A LOSS OF POWER. THE PLT STATED THAT AFTER TAKEOFF & AT AN INDICATED AIRSPEED OF 100 TO 110 MPH, AT AN ALTITUDE OF 50 FT, THE ACFT ENG STARTED TO LOSE POWER. HE DECIDED TO RETURN TO THE AIRPORT AND THE ACFT STARTED TO STALL WHILE IN THE TURN CRASHING INTOAN OPEN DITCH NEAR THE END OF THE RWY. INVESTIGATION SHOWED A DISCREPANCY OF THE FUEL NOZZLES IN THE NO. 4 CYLINDER WHICH WERE FOUND BLOCKED. THE SERVO FUEL INJECTOR HAD WATER IN THE FUEL CHAMBER & THE FUEL LINE FROM THE FUEL STRAINER TO FUEL CONTROL HAD WASTER MIXED WITH GASOLINE. THE PROPELLER WAS REMOVED & CHECKED NORMAL.
THE ACFT CRASHED SHORT OF THE RWY AFTER MAKING A 180 DEG TURN AFTER TAKEOFF FOLLOWING A LOSS OF POWER. THE PLT STATED THAT AFTER TAKEOFF & AT AN INDICATED AIRSPEED OF 100 TO 110 MPH, AT AN ALTITUDE OF 50 FT, THE ACFT ENG STARTED TO LOSE POWER. HE DECIDED TO RETURN TO THE AIRPORT AND THE ACFT STARTED TO STALL WHILE IN THE TURN CRASHING INTOAN OPEN DITCH NEAR THE END OF THE RWY. INVESTIGATION SHOWED A DISCREPANCY OF THE FUEL NOZZLES IN THE NO. 4 CYLINDER WHICH WERE FOUND BLOCKED. THE SERVO FUEL INJECTOR HAD WATER IN THE FUEL CHAMBER & THE FUEL LINE FROM THE FUEL STRAINER TO FUEL CONTROL HAD WASTER MIXED WITH GASOLINE. THE PROPELLER WAS REMOVED & CHECKED NORMAL.