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.
Fort Worth, TX
The flight instructor was demonstrating a landing using the manual Full-Authority Digital Engine Control (FADEC) mode. While on short final, approximately 3 to 5 feet above ground level, the helicopter quickly descended right and forward. Suspecting wind shear, the flight instructor applied corrective controls but was unable to reverse the downward motion prior to ground contact. The helicopter's left rear skid, then right rear skid, contacted the ground before the flight instructor could bring the helicopter back to a hover. A postflight examination of the helicopter revealed damage to the vertical stabilizer and tail boom.
Aircraft-Aircraft oper/perf/capability-Performance/control parameters-(general)-Not attained/maintained - C
The flight instructor was demonstrating a landing using the manual Full-Authority Digital Engine Control (FADEC) mode. While on short final, approximately 3 to 5 feet above ground level, the helicopter quickly descended right and forward. Suspecting wind shear, the flight instructor applied corrective controls, but was unable to reverse the downward motion prior to ground contact. The helicopter's left rear skid contacted the ground followed by the right rear skid before the flight instructor could bring the helicopter back to a hover. A post-flight examination of the helicopter revealed damage to the vertical stabilizer and tail boom.