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.
St. Augustine, FL
DURING GROUND ROLL, WITNESSES REPORTED ENG DEVELOPING INTERMITTENT POWER. TAKEOFF CONTINUED & AT ABOUT 150 FEET AGL. PLT INITIATED A TURN TO THE LEFT TO RETURN TO THE ARPT.DURING THE TURN ACFT STALLED & CRASHED ON ARPT PROPERTY. PLT WAS REMOVED FROM BURNING ACFT & TRANSPORTED TO THE HOSPITAL WHERE HE DIED OF HIS INJURIES. FIRE EXTINGUISHED BY LOCAL FIRE DEPT. EXAM OF ACFT REVEALED NO EVIDENCE OF FAILURE OR MALFUNCTION OF THE FLT CONTROLS. EXAM OF ENG REVEALED NO DETERMINATION COULD BE MADE FOR THE REPORTED INTERMITTENT POWER. THE IGNITION HARNESS & LT MAGNETO WERE DAMAGED BY FIRE. RT MAGNETO OPERATED NORMALLY, AS DID THE SPARK PLUGS. MAGNETO SWITCH AT ACCIDENT SITE POSITIONED TO THE RT MAG. IT TESTED NORMALLY. FUEL CONTINUITY FROM EACH FUEL TANK TO GASCOLATOR WAS VERIFIED. FUEL LINE FROM GASCOLATOR TO CARBURETOR WAS DAMAGED BY FIRE. EXAM OF CARBURETOR REVEALED FLOAT DESTROYED & PRIMARY VENTURI NOT INSTALLED. IDENTICAL ENG AT MANUFACTURERS FACILITY WITH VENTURI REMOVED FROM CARB REVEALED NO DEGRADATION OF ENG PERFORMANCE.
THE PILOT FAILED TO MAINTAIN AIRSPEED DURING THE TURN TO RETURN TO THE AIRPORT, RESULTING IN THE LOSS OF CONTROL. CONTRIBUTING TO THE ACCIDENT WAS HIS CONTINUED TAKEOFF WITH INTERMITTENT ENGINE POWER.
DURING GROUND ROLL, WITNESSES REPORTED ENG DEVELOPING INTERMITTENT POWER. TAKEOFF CONTINUED & AT ABOUT 150 FEET AGL. PLT INITIATED A TURN TO THE LEFT TO RETURN TO THE ARPT.DURING THE TURN ACFT STALLED & CRASHED ON ARPT PROPERTY. PLT WAS REMOVED FROM BURNING ACFT & TRANSPORTED TO THE HOSPITAL WHERE HE DIED OF HIS INJURIES. FIRE EXTINGUISHED BY LOCAL FIRE DEPT. EXAM OF ACFT REVEALED NO EVIDENCE OF FAILURE OR MALFUNCTION OF THE FLT CONTROLS. EXAM OF ENG REVEALED NO DETERMINATION COULD BE MADE FOR THE REPORTED INTERMITTENT POWER. THE IGNITION HARNESS & LT MAGNETO WERE DAMAGED BY FIRE. RT MAGNETO OPERATED NORMALLY, AS DID THE SPARK PLUGS. MAGNETO SWITCH AT ACCIDENT SITE POSITIONED TO THE RT MAG. IT TESTED NORMALLY. FUEL CONTINUITY FROM EACH FUEL TANK TO GASCOLATOR WAS VERIFIED. FUEL LINE FROM GASCOLATOR TO CARBURETOR WAS DAMAGED BY FIRE. EXAM OF CARBURETOR REVEALED FLOAT DESTROYED & PRIMARY VENTURI NOT INSTALLED. IDENTICAL ENG AT MANUFACTURERS FACILITY WITH VENTURI REMOVED FROM CARB REVEALED NO DEGRADATION OF ENG PERFORMANCE.