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.
Bakersfield, CA
THE CERTIFICATED AIRLINE TRANSPORT PILOT AND A PASSENGER DEPARTED AN INTERMEDIATE FUEL STOP DURING A FERRY FLIGHT TO DELIVER THE AIRPLANE TO A NEW OWNER. AFTER TAKEOFF, THE PILOT SMELLED FUEL AND NOTICED FUEL DRIPPING INTO THE COCKPIT FROM UNDER THE INSTRUMENT PANEL. THE PILOT RETURNED TO THE DEPARTURE AIRPORT AND DURING THE LANDING ROLL-OUT, THE ENGINE QUIT. AFTER ROLLING OFF THE ACTIVE PORTION OF THE RUNWAY, THE PILOT ATTEMPTED TO RESTART THE ENGINE. FLAMES ERUPTED IN THE ENGINE AND COCKPIT. INVESTIGATION REVEALED THAT THE FLARED END OF A COPPER FUEL PRESSURE LINE FROM THE FUEL METERING UNIT TO THE FUEL PRESSURE GAGE WAS FRACTURED DUE TO IMPROPER INSTALLATION AND OVERTORQUE. THIS CONDITION ALLOWED FUEL TO DRIP ONTO THE ALTERNATE-AIR CONTROL CABLE, RUN THROUGH THE FIREWALL TO THE INSTRUMENT PANEL AND THEN DRIP INTO THE COCKPIT.
THE PILOT'S ATTEMPT TO RESTART THE ENGINE WHEN THERE WAS EVIDENCE OF A FUEL LEAK. A FACTOR IN THE ACCIDENT WAS THE FRACTURED FUEL LINE DUE TO THE IMPROPER INSTALLATION AND OVERTORQUE OF THE LINE BY COMPANY MAINTENANCE.
THE CERTIFICATED AIRLINE TRANSPORT PILOT AND A PASSENGER DEPARTED AN INTERMEDIATE FUEL STOP DURING A FERRY FLIGHT TO DELIVER THE AIRPLANE TO A NEW OWNER. AFTER TAKEOFF, THE PILOT SMELLED FUEL AND NOTICED FUEL DRIPPING INTO THE COCKPIT FROM UNDER THE INSTRUMENT PANEL. THE PILOT RETURNED TO THE DEPARTURE AIRPORT AND DURING THE LANDING ROLL-OUT, THE ENGINE QUIT. AFTER ROLLING OFF THE ACTIVE PORTION OF THE RUNWAY, THE PILOT ATTEMPTED TO RESTART THE ENGINE. FLAMES ERUPTED IN THE ENGINE AND COCKPIT. INVESTIGATION REVEALED THAT THE FLARED END OF A COPPER FUEL PRESSURE LINE FROM THE FUEL METERING UNIT TO THE FUEL PRESSURE GAGE WAS FRACTURED DUE TO IMPROPER INSTALLATION AND OVERTORQUE. THIS CONDITION ALLOWED FUEL TO DRIP ONTO THE ALTERNATE-AIR CONTROL CABLE, RUN THROUGH THE FIREWALL TO THE INSTRUMENT PANEL AND THEN DRIP INTO THE COCKPIT.