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.
Bend, OR
THE PILOT REPORTED THAT AT TAKEOFF, THE CEILING WAS 350 FEET AGL AND VISIBILITY WAS TWO MILES. THE FLIGHT TOOK OFF AND HEADED NORTH AT AN ALTITUDE OF 250 FEET AGL, FOLLOWING A HIGHWAY. APPROXIMATELY SEVEN MILES INTO THE FLIGHT, THE CEILING AND VISIBILITY DETERIORATED AND THE PILOT INITIATED A MEDIUM BANK TURN TO THE LEFT. DURING THE TURN, THE AIRSPEED DECLINED AND THE LOW ROTOR RPM HORN SOUNDED. THE PILOT LOWERED THE NOSE AND INCREASED COLLECTIVE. DUE TO THE CLOSENESS OF THE TREES, THE PILOT ESTABLISHED THE BEST RATE OF DESCENT AND 'MILKED' THE RPM FOR A LANDING ON THE HIGHWAY. THE PILOT WAS UNABLE TO EXECUTE THE PROPER POWER OFF LANDING PROCEDURE AND THE HELICOPTER LANDED HARD. THE SKIDS COLLAPSED AND THE HELICOPTER ROLLED ONTO ITS LEFT SIDE.
ROTOR RPM WAS NOT MAINTAINED. FACTORS TO THE ACCIDENT WERE: LOW CEILING AND POOR INFLIGHT PLANNING.
THE PILOT REPORTED THAT AT TAKEOFF, THE CEILING WAS 350 FEET AGL AND VISIBILITY WAS TWO MILES. THE FLIGHT TOOK OFF AND HEADED NORTH AT AN ALTITUDE OF 250 FEET AGL, FOLLOWING A HIGHWAY. APPROXIMATELY SEVEN MILES INTO THE FLIGHT, THE CEILING AND VISIBILITY DETERIORATED AND THE PILOT INITIATED A MEDIUM BANK TURN TO THE LEFT. DURING THE TURN, THE AIRSPEED DECLINED AND THE LOW ROTOR RPM HORN SOUNDED. THE PILOT LOWERED THE NOSE AND INCREASED COLLECTIVE. DUE TO THE CLOSENESS OF THE TREES, THE PILOT ESTABLISHED THE BEST RATE OF DESCENT AND 'MILKED' THE RPM FOR A LANDING ON THE HIGHWAY. THE PILOT WAS UNABLE TO EXECUTE THE PROPER POWER OFF LANDING PROCEDURE AND THE HELICOPTER LANDED HARD. THE SKIDS COLLAPSED AND THE HELICOPTER ROLLED ONTO ITS LEFT SIDE.