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.
Fullerton, CA
THE PILOT STATED HE DEPARTED WITH 35 GALLONS OF FUEL. FLEW FOR ONE HOUR AND FIFTEEN MINUTES DURING WHICH TIME HE FLEW HALF AND HALF ON THE TANKS. HE STATED HE DEPARTED AND LANDED ON THE LEFT TANK. POST CRASH EXAMINATION OF THE FUEL SYSTEM NOTED 15 GALLONS IN THE RIGHT TANK AND 1/4 GALLON IN THE LEFT TANK. ALSO NOTED WAS A FIELD FABRICATED SECONDARY POINTER ON THE FUEL SELECTOR. THIS POINTER WOULD NOT CONSISTENTLY INDEX WITH THE STOCK IMPERIAL VALVE POINTER.
FUEL STARVATION DUE TO THE PILOT'S IMPROPER FUEL MANAGEMENT TECHNIQUE. A FACTOR WAS THE IMPROPERLY MODIFIED FUEL SELECTOR VALVE.
THE PILOT STATED HE DEPARTED WITH 35 GALLONS OF FUEL. FLEW FOR ONE HOUR AND FIFTEEN MINUTES DURING WHICH TIME HE FLEW HALF AND HALF ON THE TANKS. HE STATED HE DEPARTED AND LANDED ON THE LEFT TANK. POST CRASH EXAMINATION OF THE FUEL SYSTEM NOTED 15 GALLONS IN THE RIGHT TANK AND 1/4 GALLON IN THE LEFT TANK. ALSO NOTED WAS A FIELD FABRICATED SECONDARY POINTER ON THE FUEL SELECTOR. THIS POINTER WOULD NOT CONSISTENTLY INDEX WITH THE STOCK IMPERIAL VALVE POINTER.