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.
La Jolla, CA
THE PLT WAS QUALIFIED FOR SOLO WINCH LAUNCHES IN AN SGS-1-26 GLIDER. ON HIS 1ST WINCH LAUNCH USING A C.G. HOOK IN THIS GLIDER, HE ALLOWED THE ACFT TO ENTER AN ABNORMALLY HIGH ANGLE OF ATTACK, WHICH WAS OBSERVED THRU-OUT THE TAKEOFF PROCESS. THE GLIDE THEN ENTERED A STALL-SPIN & CRASHED. ACCORDING TO THE OWNER'S MANUAL, FORWARD ELEVATOR MUST BE USED AFTER LEAVING THE GROUND DUE TO THE LOCATION OF THE TOW HOOK & THE TENDENCY OF THE GLIDER TO ENTER A STEEP NOSE-UP ATTITUDE. THE MANUAL REQUIRED PRONOUNCED FORWARD PRESSURE THRU-OUT THE TRANSITION ARC.
THE PLT WAS QUALIFIED FOR SOLO WINCH LAUNCHES IN AN SGS-1-26 GLIDER. ON HIS 1ST WINCH LAUNCH USING A C.G. HOOK IN THIS GLIDER, HE ALLOWED THE ACFT TO ENTER AN ABNORMALLY HIGH ANGLE OF ATTACK, WHICH WAS OBSERVED THRU-OUT THE TAKEOFF PROCESS. THE GLIDE THEN ENTERED A STALL-SPIN & CRASHED. ACCORDING TO THE OWNER'S MANUAL, FORWARD ELEVATOR MUST BE USED AFTER LEAVING THE GROUND DUE TO THE LOCATION OF THE TOW HOOK & THE TENDENCY OF THE GLIDER TO ENTER A STEEP NOSE-UP ATTITUDE. THE MANUAL REQUIRED PRONOUNCED FORWARD PRESSURE THRU-OUT THE TRANSITION ARC.