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.
Anahuac, TX
The pilot had just installed a new trim system in the gyroplane and intended to complete a maintenance test flight. During the test flight, the pilot tried to adjust the trim, but nothing happened. The pilot actuated the trim switch again, and the gyroplane pitched up violently. The pilot attempted to override the trim switch but was unable to do so, and the gyroplane rapidly descended from 50 ft to ground impact. The pilot reported after the accident that a trim limit switch was not installed and that the trim system maintenance was probably done incorrectly. Thus, given the available evidence for this investigation, the pilot’s incorrect trim system maintenance likely caused the malfunction during flight and led to the pilot’s loss of gyroplane control.
The pilot’s incorrect trim system installation, which resulted in a loss of gyroplane control and impact with terrain.
On August 7, 2021, about 1115 central daylight time, an unregistered Rotary Air Force RAF 2000 gyroplane sustained substantial damage when it was involved in an accident near Anahuac, Texas. The pilot was uninjured, and the passenger sustained minor injuries. The flight was operated as a Title 14 Code of Federal Regulations Part 91 test flight. The pilot reported that the test flight occurred after a new trim system was installed. The pilot stated that, during the test flight, he tried to adjust the trim, but nothing happened. He actuated the trim switch again, and the gyroplane responded with a “massive pitch up.” He attempted to override the trim switch but was unable to do so, and the gyroplane descended rapidly from 50 ft to ground impact. The figure below shows the gyroplane on its right side in a field. The fuselage, empennage, and rotor blades sustained substantial damage. Figure. Gyroplane wreckage in its resting location (source: Texas Department of Public Safety). The pilot stated that a trim limit switch was not installed, and that the trim system maintenance was “probably” done incorrectly, which is what caused the malfunction during flight. The maintenance logbooks were not made available during the investigation.