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.
Mar Vista, CA
THE ENGINE'S NUMBER 5 INTAKE VALVE SEAT BACKED OUT OF THE HEAD IMMEDIATELY AFTER TAKEOFF, RESULTING IN THE LOSS OF POWER OF 3 CYLINDERS. THE PILOT ENTERED A TURN TO RETURN TO THE RUNWAY. THE AIRCRAFT STALLED AND COLLIDED WITH A RESIDENCE. THE AIRCRAFT FLIGHT MANUAL RECOMMENDED A STRAIGHT AHEAD FLIGHT PATH IN THE EVENT OF A POWER LOSS. THE REMAINING 9 CYLINDERS WERE PRODUCING SUFFICIENT POWER TO ENABLE THE AIRCRAFT TO SLOWLY CLIMB ON A STRAIGHT AHEAD FLIGHT PATH.
THE PILOT'S POOR IN-FLIGHT PLANNING IN ATTEMPTING TO IMMEDIATELY RETURN TO THE AIRPORT AND NOT FOLLOWING ESTABLISHED PROCEDURES AFTER THE LOSS OF POWER AFTER TAKEOFF. THE FAILURE OF AN INTAKE VALVE WAS A FACTOR IN THE ACCIDENT.
THE ENGINE'S NUMBER 5 INTAKE VALVE SEAT BACKED OUT OF THE HEAD IMMEDIATELY AFTER TAKEOFF, RESULTING IN THE LOSS OF POWER OF 3 CYLINDERS. THE PILOT ENTERED A TURN TO RETURN TO THE RUNWAY. THE AIRCRAFT STALLED AND COLLIDED WITH A RESIDENCE. THE AIRCRAFT FLIGHT MANUAL RECOMMENDED A STRAIGHT AHEAD FLIGHT PATH IN THE EVENT OF A POWER LOSS. THE REMAINING 9 CYLINDERS WERE PRODUCING SUFFICIENT POWER TO ENABLE THE AIRCRAFT TO SLOWLY CLIMB ON A STRAIGHT AHEAD FLIGHT PATH.