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.
Grand Isle, LA
THE PILOT WAS APPROACHING AN OFFSHORE PLATFORM FOR LANDING AT ABOUT 100 FT AGL WHEN HE FELT THE HELICOPTER SHUDDER. HE ALSO HEARD AN ENGINE-OUT HORN AND A LOW-ROTOR-RPM WARNING. HE TURNED AWAY FROM THE PLATFORM, POPPED THE EMERGENCY FLOATS AND INITIATED AN AUTOROTATIVE LANDING. HOWEVER, THE FLOATS WERE NOT YET FULLY INFLATED AT THE TIME OF WATER CONTACT AND THE HELICOPTER IMMEDIATELY FLIPPED INVERTED. AN EXAMINATION REVEALED THAT THE OUTER SHAFT IN THE FREE-WHEELING UNIT HAD FAILED AT THE SPLINE AREA. THIS ALLOWED THE ENGINE TO GO INTO AN OVERSPEED. THEN AUTOMATICALLY SHUT DOWN.
THE PILOT WAS APPROACHING AN OFFSHORE PLATFORM FOR LANDING AT ABOUT 100 FT AGL WHEN HE FELT THE HELICOPTER SHUDDER. HE ALSO HEARD AN ENGINE-OUT HORN AND A LOW-ROTOR-RPM WARNING. HE TURNED AWAY FROM THE PLATFORM, POPPED THE EMERGENCY FLOATS AND INITIATED AN AUTOROTATIVE LANDING. HOWEVER, THE FLOATS WERE NOT YET FULLY INFLATED AT THE TIME OF WATER CONTACT AND THE HELICOPTER IMMEDIATELY FLIPPED INVERTED. AN EXAMINATION REVEALED THAT THE OUTER SHAFT IN THE FREE-WHEELING UNIT HAD FAILED AT THE SPLINE AREA. THIS ALLOWED THE ENGINE TO GO INTO AN OVERSPEED. THEN AUTOMATICALLY SHUT DOWN.