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.
Flagstaff, AZ
The pilot reported that he was landing the helicopter in a bowl-shaped meadow surrounded by mountains and trees. While circling the landing zone to determine the surface wind and descending, about 20 feet above ground level, the helicopter encountered a wind gust. The low rotor horn sounded and the pilot regained rpm, but another wind gust from behind again resulted in a loss of rotor rpm. The pilot said he was too low to recover, so he performed a run-on landing. The helicopter struck an earthen berm and rolled onto its left side, which resulted in substantial damage to the fuselage and tail boom. The elevation at the accident site was 8,411 feet; the density altitude was calculated to have been 10,059 feet. The pilot reported no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation.
Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Prop/rotor parameters-Not attained/maintained - C
The pilot reported that he was landing the helicopter in a bowl-shaped meadow surrounded by mountains and trees. While circling the landing zone to determine the surface winds and descending, about 20 feet above ground level, the helicopter encountered a wind gust. The low rotor horn sounded and the pilot regained rpm, but another wind gust from behind again resulted in a loss of rotor rpm. The pilot said he was too low to recover, so he performed a run-on landing. The helicopter struck an earthen berm and rolled onto its left side, which resulted in substantial damage to the fuselage and tail boom. The elevation at the accident site was 8,411 feet; the density altitude was calculated to have been 10,059 feet. The pilot reported no preimpact mechanical malfunctions or failures with the helicopter that would have precluded normal operation.