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.
Camarillo, CA
On the landing rollout, the airplane departed the runway and came to rest inverted in an adjacent field. The adjacent field had recently been plowed and contained furrows. The airplane traveled perpendicular to the furrows and nosed over. The purpose of the flight was to practice maneuvers and fulfill the experimental operating certificate limitations initial 40-hour requirement. The pilot had accrued 5 hours of flight time on the airplane. When he returned to land, he noted a crosswind but did not believe that it would have an effect on the landing. There were no mechanical anomalies noted with the airplane by the pilot. Of note in the pilot's written statement was the directional instability that he encountered during takeoffs in the 7 hours that were placed on the airplane within the previous year. He made several modifications, mostly rigging changes to the tailwheel, to improve the takeoff characteristics. While in contact with the Sonerai technical representative, the owner stated that there were plans to convert the conventional landing gear airplane to a tricycle landing gear. The proposed modification would solve the instability problem.
Failure of the pilot to maintain directional control on the landing rollout. Factors were the owner/pilot's inadequate remedial design changes and the freshly plowed field.
On December 17, 2001, about 1250 Pacific standard time, a Vernon Sonerai II, N6399D, lost directional control on the landing rollout on runway 26, and came to rest inverted in an adjacent field at the Camarillo Airport, Camarillo, California. The experimental airplane was operated by the owner under the provisions of 14 CFR Part 91, and sustained substantial damage. The private pilot, the sole occupant, was not injured. Visual meteorological conditions prevailed for the local area flight and no flight plan had been filed. The airplane departed Camarillo about 1000. The Safety Board investigator interviewed the pilot. The pilot stated that the purpose of the flight was to practice maneuvers, as well as to fulfill the experimental certificate operating limitations initial 40-hour requirement. He indicated that he had accrued 5 hours of flight time in the airplane, which was also the total time on the airplane. After departing Camarillo airspace, the pilot flew towards Santa Paula, about 10 miles away, to practice maneuvers. He flew about 1.5 hours before returning to Camarillo for landing. He noted a slight crosswind on landing, but nothing unusual. In the pilot's written statement to the Safety Board, he stated that after touchdown the airplane became directionally unstable with increasing amplitude until the airplane was facing perpendicular to the runway. The airplane then departed the runway, and traveled perpendicular to the furrows present in the infield of the airport. Of note in the pilot's written statement was the directional instability that he encountered during takeoffs in the 7 hours that were placed on the airplane. He made several modifications, mostly rigging changes to the tail wheel, to improve the takeoff characteristics. While in contact with the Sonerai technical representative, the owner stated that there were plans to convert the conventional landing gear airplane to a tricycle landing gear. The proposed modification would solve the instability problem, "the resulting mass induced control signals are stabilizing instead of destabilizing."