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.
Sandy, OR
THE ENGINE LOST POWER SHORTLY AFTER TAKEOFF AND A FORCED LANDING WAS MADE IN AN OPEN FIELD. THE AIRPLANE COLLIDED WITH THE TERRAIN AND CARTWHEELED. THE BOLT CONNECTING THE THROTTLE ARM TO THE THROTTLE ROD END WAS MISSING. A BOLT IDENTIFIED AS THE PROPER TYPE FOR THIS CONNECTION WAS FOUND LAYING AGAINST THE FIREWALL. THE BOLT IS SUPPOSDE TO BE SECURED WITH A CASTELLATED NUT AND A COTTER PIN. NEITHER THE NUT NOR THE COTTER PIN WAS FOUND. THE BOLT WAS NOT DAMAGED.AN ANNUAL INSPECTION WAS PERFORMED 5 FLIGHT HOURS PRIOR TO THE ACCIDENT. THE OPEN FIELD USED FOR THE FORCED LANDING IS SURROUNDED BY 100 FT TREES, WITH BARBED WIRE FENCES 300 TO 400 FT APART. INITIAL GROUND IMPACT MARK WAS LOCATED 64 INCHES FROM A FENCE.
THE LOSS OF ENGINE POWER DUE TO THE SEPARATION OF THE BOLT CONNECTING THE THROTTLE ROD TO THE CARBURETOR THROTTLE ARM AND AN INADEQUATE ANNUAL INSPECTION PERFORMED 5 FLIGHT HOURS PRIOR TO THE OCCURRENCE. CONTRIBUTING FACTORS WERE OBSTRUCTIONS IN AND AROUND THE ONLY OPEN FIELD AVAILABLE FOR THE FORCED LANDING.
THE ENGINE LOST POWER SHORTLY AFTER TAKEOFF AND A FORCED LANDING WAS MADE IN AN OPEN FIELD. THE AIRPLANE COLLIDED WITH THE TERRAIN AND CARTWHEELED. THE BOLT CONNECTING THE THROTTLE ARM TO THE THROTTLE ROD END WAS MISSING. A BOLT IDENTIFIED AS THE PROPER TYPE FOR THIS CONNECTION WAS FOUND LAYING AGAINST THE FIREWALL. THE BOLT IS SUPPOSDE TO BE SECURED WITH A CASTELLATED NUT AND A COTTER PIN. NEITHER THE NUT NOR THE COTTER PIN WAS FOUND. THE BOLT WAS NOT DAMAGED.AN ANNUAL INSPECTION WAS PERFORMED 5 FLIGHT HOURS PRIOR TO THE ACCIDENT. THE OPEN FIELD USED FOR THE FORCED LANDING IS SURROUNDED BY 100 FT TREES, WITH BARBED WIRE FENCES 300 TO 400 FT APART. INITIAL GROUND IMPACT MARK WAS LOCATED 64 INCHES FROM A FENCE.