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.
Goliad, TX
THE PILOT, WHO HAD BORROWED THE AIRPLANE REPORTED THAT HE WAS IN CRUISE FLIGHT AT 1,500 FEET MSL, LOOKING AT PROPERTY, WHEN THE ENGINE BACKFIRED AND STARTED TO 'SPUTTER.' SWITCHING TANKS AND APPLYING CARBURETOR HEAT FOR AN UNDETERMINED TIME DID NOT ALLEVIATE THE PROBLEM. THE PILOT ELECTED TO EXECUTE A PRECAUTIONARY LANDING ON A RANCH ROAD. DURING THE LANDING ROLL, THE RIGHT WING STRUCK A TREE AND VEERED RIGHT, CAUSING THE LEFT WING TO STRIKE THE GROUND. THE OWNER RECOVERED THE AIRPLANE AND STATED THAT THE ENGINE OPERATED NORMALLY THROUGHOUT 2 STARTS, RUN UPS, AND THE SUBSEQUENT TAKEOFF AND FLIGHT. THE TEMPERATURE/DEW POINT CONDITIONS THAT EXISTED AT THE TIME OF THE ACCIDENT WERE CONDUCIVE TO THE FORMATION OF CARBURETOR ICE AT CRUISE AND GLIDE POWER SETTINGS.
THE PILOT IN COMMAND'S FAILURE TO IDENTIFY AND CORRECT FOR CARBURETOR ICING CONDITIONS WHICH EXISTED AT THE TIME OF THE ACCIDENT AND PRECIPITATED THE PRECAUTIONARY LANDING.
THE PILOT, WHO HAD BORROWED THE AIRPLANE REPORTED THAT HE WAS IN CRUISE FLIGHT AT 1,500 FEET MSL, LOOKING AT PROPERTY, WHEN THE ENGINE BACKFIRED AND STARTED TO 'SPUTTER.' SWITCHING TANKS AND APPLYING CARBURETOR HEAT FOR AN UNDETERMINED TIME DID NOT ALLEVIATE THE PROBLEM. THE PILOT ELECTED TO EXECUTE A PRECAUTIONARY LANDING ON A RANCH ROAD. DURING THE LANDING ROLL, THE RIGHT WING STRUCK A TREE AND VEERED RIGHT, CAUSING THE LEFT WING TO STRIKE THE GROUND. THE OWNER RECOVERED THE AIRPLANE AND STATED THAT THE ENGINE OPERATED NORMALLY THROUGHOUT 2 STARTS, RUN UPS, AND THE SUBSEQUENT TAKEOFF AND FLIGHT. THE TEMPERATURE/DEW POINT CONDITIONS THAT EXISTED AT THE TIME OF THE ACCIDENT WERE CONDUCIVE TO THE FORMATION OF CARBURETOR ICE AT CRUISE AND GLIDE POWER SETTINGS.