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.
Tomball, TX
THE AIRPLANE EXPERIENCED A COMPLETE LOSS OF ENGINE POWER DUE TO FUEL EXHAUSTION ON AN EXTENDED DOWNWIND AFTER A TWO LEG CROSS COUNTRY FLIGHT, WHICH LASTED 2.9 HOURS. THE SECOND PILOT EXECUTED A NIGHT FORCED LANDING AS HE HAD MORE TOTAL TIME THAN THE PIC. DURING THE LANDING ROLL, THE AIRPLANE ENCOUNTERED SOFT/WET TERRAIN, THE NOSE GEAR PARTIALLY COLLAPSED, AND THE AIRPLANE FLIPPED OVER. INVESTIGATION REVEALED THAT THE RENTAL AIRPLANE HAD FLOWN 1 FLIGHT OF 0.7 HRS BEFORE DEPARTING ON THE ACCIDENT TRIP AND HAD NOT BEEN REFUELED ON ITS RETURN. THE PIC HAD BASED HER FUEL CONSUMPTION CALCULATIONS ON A RATE OF 4.6 GPH INSTEAD OF THE 6.4 GPH THAT RECORDS INDICATED WAS THE CORRECT CONSUMPTION RATE.
THE PILOT IN COMMAND'S INACCURATE FUEL CONSUMPTION CALCULATIONS, WHICH RESULTED IN LOSS OF ENGINE POWER DUE TO FUEL EXHAUSTION. FACTORS IN THIS ACCIDENT WERE: THE DARK NIGHT, AND THE SOFT/WET TERRAIN.
THE AIRPLANE EXPERIENCED A COMPLETE LOSS OF ENGINE POWER DUE TO FUEL EXHAUSTION ON AN EXTENDED DOWNWIND AFTER A TWO LEG CROSS COUNTRY FLIGHT, WHICH LASTED 2.9 HOURS. THE SECOND PILOT EXECUTED A NIGHT FORCED LANDING AS HE HAD MORE TOTAL TIME THAN THE PIC. DURING THE LANDING ROLL, THE AIRPLANE ENCOUNTERED SOFT/WET TERRAIN, THE NOSE GEAR PARTIALLY COLLAPSED, AND THE AIRPLANE FLIPPED OVER. INVESTIGATION REVEALED THAT THE RENTAL AIRPLANE HAD FLOWN 1 FLIGHT OF 0.7 HRS BEFORE DEPARTING ON THE ACCIDENT TRIP AND HAD NOT BEEN REFUELED ON ITS RETURN. THE PIC HAD BASED HER FUEL CONSUMPTION CALCULATIONS ON A RATE OF 4.6 GPH INSTEAD OF THE 6.4 GPH THAT RECORDS INDICATED WAS THE CORRECT CONSUMPTION RATE.