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.
Portland, ME
THE AIRPLANE WAS ON A FERRY FLIGHT WITH AN AUXILIARY FUEL TANK IN THE FUSELAGE FOR INCREASED RANGE. DURING FUEL TRANSFER FROM THE AUXILIARY TANK TO THE MAIN WING TANK, THE FUEL PRESSURE BECAME EXCESSIVE AND THE WING TANK RUPTURED. THE PILOT SAID THE FUEL QUANTITY GAUGE WAS INACCURATE. THE WING TANK VENT SYSTEM WAS NOT ADEQUATE TO HANDLE THE EXCESSIVE FUEL BEING SUPPLIED BY THE AUXILIARY TANK. THE PILOT EXPERIENCED SOME FLIGHT CONTROL DIFFICULTY AFTER THE RUPTURE, BUT HE MANAGED TO LAND WITHOUT INCIDENT.
THE EXCESSIVE FUEL PRESSURE DURING INFLIGHT FUEL TRANSFERRING, WHICH RESULTED IN THE RUPTURE OF THE WING TANK AND SUBSEQUENT DAMAGE TO THE WING. ALSO CAUSAL TO THE ACCIDENT WAS THE INADEQUATE FUEL TANK VENT SYSTEM AND THE INACCURATE FUEL QUANTITY SYSTEM.
THE AIRPLANE WAS ON A FERRY FLIGHT WITH AN AUXILIARY FUEL TANK IN THE FUSELAGE FOR INCREASED RANGE. DURING FUEL TRANSFER FROM THE AUXILIARY TANK TO THE MAIN WING TANK, THE FUEL PRESSURE BECAME EXCESSIVE AND THE WING TANK RUPTURED. THE PILOT SAID THE FUEL QUANTITY GAUGE WAS INACCURATE. THE WING TANK VENT SYSTEM WAS NOT ADEQUATE TO HANDLE THE EXCESSIVE FUEL BEING SUPPLIED BY THE AUXILIARY TANK. THE PILOT EXPERIENCED SOME FLIGHT CONTROL DIFFICULTY AFTER THE RUPTURE, BUT HE MANAGED TO LAND WITHOUT INCIDENT.