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.
Merritt Island, FL
WHILE CHECKING THE STALL CHARACTERISTICS OF A HOMEBUILT ACFT, THE ACFT DESCENDED IN A STALLED CONDITION UNTIL CRASHING INTO A RIVER. THE PLT WAS UNABLE TO LOWER THE NOSE. INVESTIGATION REVEALED THAT HE IMPROPERLY POSITIONED BAFFLES IN THE FUEL TANKS RESULTING IN AN INCREASE OF 20 GALLONS. IF THE ANGLE OF ATTACK WERE NOSE HIGH FUEL WOULD SHIFT AFT RESULTING IN AN OUT OF LIMIT AFT C.G. THE FUSELAGE HAD BEEN IMPROPERLY LEVELLED RESULTING IN A NOSE HIGH ATTITUDE. AS A RESULT THE POSITION OF THE AIRFOIL SHAPED TANKS LOCATED FWD OF EACH WING & BONDED TO THE FUSELAGE WERE IMPROPERLY POSITIONED. THE FUEL TANKS ARE PART OF THE WING & PROVIDE LIFT. THIS MOVED THE CENTER OF LIFT FWD, & WITH THE AFT SHIFTING OF FUEL RESULTED IN THE NOSE HIGH DESCENT. ACCORDING TO A PLT WHO HAS FLOWN A SIMILARLY DESIGNED ACFT, DURING FLT TESTING IT STALLED & DESCENDED IN THE SAME ATTITUDE OF THE ACCIDENT ACFT. RECOVERY OCCURRED WHEN HE ADDED AND MAINTAINED FULL POWER.
WHILE CHECKING THE STALL CHARACTERISTICS OF A HOMEBUILT ACFT, THE ACFT DESCENDED IN A STALLED CONDITION UNTIL CRASHING INTO A RIVER. THE PLT WAS UNABLE TO LOWER THE NOSE. INVESTIGATION REVEALED THAT HE IMPROPERLY POSITIONED BAFFLES IN THE FUEL TANKS RESULTING IN AN INCREASE OF 20 GALLONS. IF THE ANGLE OF ATTACK WERE NOSE HIGH FUEL WOULD SHIFT AFT RESULTING IN AN OUT OF LIMIT AFT C.G. THE FUSELAGE HAD BEEN IMPROPERLY LEVELLED RESULTING IN A NOSE HIGH ATTITUDE. AS A RESULT THE POSITION OF THE AIRFOIL SHAPED TANKS LOCATED FWD OF EACH WING & BONDED TO THE FUSELAGE WERE IMPROPERLY POSITIONED. THE FUEL TANKS ARE PART OF THE WING & PROVIDE LIFT. THIS MOVED THE CENTER OF LIFT FWD, & WITH THE AFT SHIFTING OF FUEL RESULTED IN THE NOSE HIGH DESCENT. ACCORDING TO A PLT WHO HAS FLOWN A SIMILARLY DESIGNED ACFT, DURING FLT TESTING IT STALLED & DESCENDED IN THE SAME ATTITUDE OF THE ACCIDENT ACFT. RECOVERY OCCURRED WHEN HE ADDED AND MAINTAINED FULL POWER.