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.
Labelle, FL
THE PRIVATE PILOT DEPARTED ON A VFR FLIGHT IN VFR CONDITIONS. A WITNESS OBSERVED THE HELICOPTER AT ABOUT 600 FEET AGL DESCENDING IN AN AUTOROTATION WITH A HIGH RATE OF DESCENT, FORWARD AIRSPEED, WITH THE NOSE PITCHED UP ABOUT 45 DEGREES BEFORE THE HELICOPTER DISAPPEARED BELOW THE TREE LINE. EXAMINATION OF THE CRASH SITE REVEALED THE HELICOPTER COLLIDED WITH TREES IN A DESCENDING LEFT TURN PRIOR TO IMPACTING THE GROUND IN ABOUT A 45-DEGREE NOSE DOWN ATTITUDE, NOSED OVER AND CAME TO REST ON ITS RIGHT SIDE. THE PILOT WAS FATALLY INJURED. CONTRIBUTING TO THE ACCIDENT WAS THE TOTAL LOSS OF ENGINE POWER DUE TO FUEL CONTAMINATION. THE DECEASED PILOT'S SON STATED THE FATHER WOULD ALLOW THE HELICOPTER TO SIT AT THE HOUSE WITHOUT A FULL TANK OF FUEL, AND THAT HIS FATHER WOULD NOT DRAIN THE FUEL SUMP AS A PART OF HIS PREFLIGHT INSPECTION.
THE PILOT-IN-COMMAND'S IMPROPER APPLICATION OF COLLECTIVE PITCH DURING AN AUTOROTATIVE LANDING RESULTING IN INSUFFICIENT ROTOR RPM AND IN-FLIGHT COLLISION WITH TREES AND THE TERRAIN. CONTRIBUTING TO THE ACCIDENT WAS THE TOTAL LOSS OF ENGINE POWER DUE TO FUEL CONTAMINATION AND INADEQUATE PREFLIGHT PLANNING/PREPARATION.
THE PRIVATE PILOT DEPARTED ON A VFR FLIGHT IN VFR CONDITIONS. A WITNESS OBSERVED THE HELICOPTER AT ABOUT 600 FEET AGL DESCENDING IN AN AUTOROTATION WITH A HIGH RATE OF DESCENT, FORWARD AIRSPEED, WITH THE NOSE PITCHED UP ABOUT 45 DEGREES BEFORE THE HELICOPTER DISAPPEARED BELOW THE TREE LINE. EXAMINATION OF THE CRASH SITE REVEALED THE HELICOPTER COLLIDED WITH TREES IN A DESCENDING LEFT TURN PRIOR TO IMPACTING THE GROUND IN ABOUT A 45-DEGREE NOSE DOWN ATTITUDE, NOSED OVER AND CAME TO REST ON ITS RIGHT SIDE. THE PILOT WAS FATALLY INJURED. CONTRIBUTING TO THE ACCIDENT WAS THE TOTAL LOSS OF ENGINE POWER DUE TO FUEL CONTAMINATION. THE DECEASED PILOT'S SON STATED THE FATHER WOULD ALLOW THE HELICOPTER TO SIT AT THE HOUSE WITHOUT A FULL TANK OF FUEL, AND THAT HIS FATHER WOULD NOT DRAIN THE FUEL SUMP AS A PART OF HIS PREFLIGHT INSPECTION.