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.
Palo Alto, CA
AFTER TAKEOFF THE FLIGHT REMAINED IN A CLOSED TRAFFIC PATTERN. ON TURN TO FINAL THE ENGINE LOST POWER AND THE AIRCRAFT LANDED IN A BAY SHORT OF THE RUNWAY. NO FUEL WAS FOUND FORWARD OF THE FIREWALL. THE FUEL STRAINER AT THE FUEL CONTROL UNIT CONTAINED SMALL DARK PARTICLES. EXAMINATION OF THE ELECTRIC FUEL PUMP REVEALED THAT THE VANES HAD DAMAGE AND SEVERELY RESTRICTED THE FLOW OF FUEL. THE MECHANICAL FUEL PUMP WAS OKAY.
A LOSS OF ENGINE POWER DUE TO FUEL STARVATION. THE FUEL STARVATION WAS THE RESULT OF VANE PARTICLES FROM THE DETERIORATED ELECTRIC FUEL PUMP RESTRICTING THE UPSTREAM FLOW OF FUEL.
AFTER TAKEOFF THE FLIGHT REMAINED IN A CLOSED TRAFFIC PATTERN. ON TURN TO FINAL THE ENGINE LOST POWER AND THE AIRCRAFT LANDED IN A BAY SHORT OF THE RUNWAY. NO FUEL WAS FOUND FORWARD OF THE FIREWALL. THE FUEL STRAINER AT THE FUEL CONTROL UNIT CONTAINED SMALL DARK PARTICLES. EXAMINATION OF THE ELECTRIC FUEL PUMP REVEALED THAT THE VANES HAD DAMAGE AND SEVERELY RESTRICTED THE FLOW OF FUEL. THE MECHANICAL FUEL PUMP WAS OKAY.