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.
Tahlequah, OK
The pilot reported the airplane had recently been purchased by the passenger and they were transporting it to their home location via a cross-country flight. During a planned rest stop, the pilot maneuvered the airplane in the traffic pattern to land. As the pilot turned onto short final, he was attempting to align the airplane with the runway, and he noticed the yaw of the airplane was to the left and “hard.” The pilot made sure the right seat passenger did not have his feet resting on the rudder pedals. The pilot noticed the left rudder pedal was all the way forward against the firewall and he was unable to free it by manipulating the rudder pedals back and forth. The pilot then decided to land parallel to the runway, in dry, tall grass. During the landing, the airplane impacted several saplings, nosed over, and came to rest inverted. The pilot and passenger were able to egress without further incident. The airplane sustained substantial damage to the left-wing lift struts, the vertical stabilizer, and the rudder. A post-accident examination of the airframe established flight control continuity and no signs of foreign object debris were found lodged in or around the rudder pedals. Pre-accident flight control rigging settings could be not determined due to the airframe damage sustained.
A loss of yaw control while on final approach, which resulted in the pilot performing an off-runway landing, and a subsequent nose over. The reason for the loss of yaw control could not be determined based on the available evidence.
The pilot reported the airplane had recently been purchased by the passenger and they were transporting it to their home location via a cross-country flight. During a planned rest stop, the pilot maneuvered the airplane in the traffic pattern to land. As the pilot turned onto short final, he was attempting to align the airplane with the runway, and he noticed the yaw of the airplane was to the left and “hard.” The pilot made sure the right seat passenger did not have his feet resting on the rudder pedals. The pilot noticed the left rudder pedal was all the way forward against the firewall and he was unable to free it by manipulating the rudder pedals back and forth. The pilot then decided to land parallel to the runway, in dry, tall grass. During the landing, the airplane impacted several saplings, nosed over, and came to rest inverted. The pilot and passenger were able to egress without further incident. The airplane sustained substantial damage to the left-wing lift struts, the vertical stabilizer, and the rudder. A post-accident examination of the airframe established flight control continuity and no signs of foreign object debris were found lodged in or around the rudder pedals. Pre-accident flight control rigging settings could be not determined due to the airframe damage sustained.