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.
Pelican, AK
The pilot reported that he was conducting helicopter external sling load operations to a remote mountain top. At the drop off site, while in a hover about 20 ft above the ground, with his attention focused outside to ensure he cleared terrain and obstacles, he felt the helicopter begin to settle. The rpm began to decay, the low rotor rpm light illuminated, and the horn sounded. He immediately lowered the collective, released the cargo and impacted the ground coming to rest on top of the cargo. The helicopter sustained substantial damage to the rotor system and vertical stabilizer. The pilot reported that there were no preaccident mechanical malfunctions or anomalies with the helicopter that would have precluded normal operation, and that the accident may have been prevented if he had received additional training from the company to include flying at gross weight with and without external loads. In addition to having pilots check for available power in an out-of-ground effect hover with altitudes and escape routes before committing to the approach.
The pilot’s improper preflight planning to ensure adequate power to hover out-of-ground effect while conducting external load operations.
The pilot reported that he was conducting helicopter external sling load operations to a remote mountain top. At the drop off site, while in a hover about 20 ft above the ground, with his attention focused outside to ensure he cleared terrain and obstacles, he felt the helicopter begin to settle. The rpm began to decay, the low rotor rpm light illuminated, and the horn sounded. He immediately lowered the collective, released the cargo and impacted the ground coming to rest on top of the cargo. The helicopter sustained substantial damage to the rotor system and vertical stabilizer. The pilot reported that there were no preaccident mechanical malfunctions or anomalies with the helicopter that would have precluded normal operation, and that the accident may have been prevented if he had received additional training from the company to include flying at gross weight with and without external loads. In addition to having pilots check for available power in an out-of-ground effect hover with altitudes and escape routes before committing to the approach.