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.
San Diego, CA
DURING FLT, THE ENG LOST POWER & THE PLT BEGAN AN AUTOROTATIVE LANDING IN A PARKING LOT. DURING THE APCH, HE MANEUVERED TO AVOID A 100 FT CRANE. AS THE HELICOPTER WAS APPROACHING THE INTENDED TOUCHDOWN POINT, A VEHICLE WAS DRIVEN INTO THE FLT PATH OF THE ACFT. TO AVOID THE VEHICLE, THE PLT INCREASED THE COLLECTIVE TO EXTEND THE GLIDE PATH. SUBSEQUENTLY, THE HELICOPTER LOST ROTOR RPM BEFORE TOUCHDOWN & LANDED HARD. AN EXAM REVEALED THAT AN IMPROPER PART (AN OIL LINE) HAD BEEN SUBSTITUTED FOR THE 'COMPRESSOR TO FUEL CONTROL PRESSURE SENSING' LINE (PN 6848471). THE LINE HAD FRACTURED AT A B-NUT WHICH RESULTED IN A LOSS OF POWER.
DURING FLT, THE ENG LOST POWER & THE PLT BEGAN AN AUTOROTATIVE LANDING IN A PARKING LOT. DURING THE APCH, HE MANEUVERED TO AVOID A 100 FT CRANE. AS THE HELICOPTER WAS APPROACHING THE INTENDED TOUCHDOWN POINT, A VEHICLE WAS DRIVEN INTO THE FLT PATH OF THE ACFT. TO AVOID THE VEHICLE, THE PLT INCREASED THE COLLECTIVE TO EXTEND THE GLIDE PATH. SUBSEQUENTLY, THE HELICOPTER LOST ROTOR RPM BEFORE TOUCHDOWN & LANDED HARD. AN EXAM REVEALED THAT AN IMPROPER PART (AN OIL LINE) HAD BEEN SUBSTITUTED FOR THE 'COMPRESSOR TO FUEL CONTROL PRESSURE SENSING' LINE (PN 6848471). THE LINE HAD FRACTURED AT A B-NUT WHICH RESULTED IN A LOSS OF POWER.