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.
Bethel, AK
THE PILOT IN COMMAND/FLIGHT INSTRUCTOR REPORTED THAT THE ENGINE BEGAN TO RUN ROUGH ABOUT TWO HOURS INTO THE FLIGHT. FULL CARBURETOR HEAT WAS APPLIED AND THE ROUGHNESS DISAPPEARED. ABOUT 30 MINUTES LATER, THE ENGINE ROUGHNESS REAPPEARED. ENGINE INSTRUMENT INDICATIONS WERE NORMAL. THE ENGINE COUGHED AND SPUTTERED, BUT LITTLE FLUCTUATION IN RPM WAS NOTED. FULL CARBURETOR HEAT WAS ONCE AGAIN APPLIED BUT THE ENGINE QUIT AND ATTEMPTS AT RESTARTING WERE NOT SUCCESSFUL. THE ENGINE STARTED AND RAN NORMALLY (RESTRICTED TO LOW RPM DUE TO MOTOR MOUNT DAMAGE) DURING A POST ACCIDENT STATIC EXAMINATION AND OPERATIONAL CHECK. ALL ENGINE CONTROLS WERE INTACT. NO FOREIGN MATERIAL/CONTAMINANTS WAS FOUND IN THE WING TANKS, ENGINE FUEL STRAINER, AND CARBURETOR FINGER SCREEN. THE TEMPERATURE/DEW POINT AT THE TIME OF THE ACCIDENT WAS 44 DEG AND 30 DEG RESPECTIVELY. ACCORDING TO THE CARB ICING PROB CHART SERIOUS ICING AT CRUISE POWER WAS POSSIBLE AT THE AMBIENT CONDITIONS.
THE CARBURETOR ICING CONDITIONS AND THE DELAY BY THE PILOT IN COMMAND/CFI IN USING CARBURETOR HEAT.
THE PILOT IN COMMAND/FLIGHT INSTRUCTOR REPORTED THAT THE ENGINE BEGAN TO RUN ROUGH ABOUT TWO HOURS INTO THE FLIGHT. FULL CARBURETOR HEAT WAS APPLIED AND THE ROUGHNESS DISAPPEARED. ABOUT 30 MINUTES LATER, THE ENGINE ROUGHNESS REAPPEARED. ENGINE INSTRUMENT INDICATIONS WERE NORMAL. THE ENGINE COUGHED AND SPUTTERED, BUT LITTLE FLUCTUATION IN RPM WAS NOTED. FULL CARBURETOR HEAT WAS ONCE AGAIN APPLIED BUT THE ENGINE QUIT AND ATTEMPTS AT RESTARTING WERE NOT SUCCESSFUL. THE ENGINE STARTED AND RAN NORMALLY (RESTRICTED TO LOW RPM DUE TO MOTOR MOUNT DAMAGE) DURING A POST ACCIDENT STATIC EXAMINATION AND OPERATIONAL CHECK. ALL ENGINE CONTROLS WERE INTACT. NO FOREIGN MATERIAL/CONTAMINANTS WAS FOUND IN THE WING TANKS, ENGINE FUEL STRAINER, AND CARBURETOR FINGER SCREEN. THE TEMPERATURE/DEW POINT AT THE TIME OF THE ACCIDENT WAS 44 DEG AND 30 DEG RESPECTIVELY. ACCORDING TO THE CARB ICING PROB CHART SERIOUS ICING AT CRUISE POWER WAS POSSIBLE AT THE AMBIENT CONDITIONS.