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.
Reidsville, GA
The airplane inadvertently entered a spin during recovery from a practice power-off stall, with 30 degrees of flaps deployed. The pilot stated that during the recovery of the practice stall he applied, "full power and nose level...the airplane went sideways and started spinning downwards." The pilot did not immediately reduce power, and the airplane's speed increased as it descended. He reported that upon recovering from the spin, the airspeed was over 120 knots; however, the airplane's maximum airspeed with flaps extended was 85 knots. The pilot subsequently retracted the flaps and heard a "creaking noise." Postaccident inspection of the airplane revealed that the wings and flaps were damaged.
Aircraft-Aircraft oper/perf/capability-Performance/control parameters-(general)-Not attained/maintained - C
The Cessna 172M inadvertently entered a spin during recovery from a practice power-off stall, with 30 degrees of flaps deployed. The pilot stated that during the recovery of the practice stall he applied, "full power and nose level...the airplane went sideways and started spinning downwards." The pilot did not immediately reduce power, and the airplane's speed increased as it descended. He reported that upon recovering from the spin, the airspeed was over 120 knots; however, the airplane's maximum airspeed with flaps extended was 85 knots. The pilot subsequently retracted the flaps and heard a "creaking noise." Post accident inspection of the airplane revealed that the wings and flaps were substantially damaged.