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.
Richmond, TX
On May 28, 2026, about 1440 central daylight time, a Mustang Aeronautics Mustang II airplane, N160MT, sustained substantial damage when it was involved in an accident near Richmond, Texas. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the pilot, he had recently purchased the experimental amateur-built airplane, and the airplane was based at the Covey Trails Airport (X09), Richmond, Texas. The airplane departed from X09 and was performing multiple touch-and-go landings to the single turf runway at the airport. While performing the multiple touch-and-go landings, the pilot reported he was utilizing the carburetor heat. During the final touch-and-go landing, just after the takeoff, the engine sustained a partial loss of power. The engine was unable to provide sufficient power to climb, and the pilot performed a forced landing. The airplane impacted a metal fence, and it came to rest upright on a flat grass field just to the south of X09 near a residential area. The airplane sustained substantial damage to the fuselage and to both wings. The pilot reported that during the recovery of the airplane from the accident site, he drained about 10 gallons of 100 low lead fuel from the fuselage fuel tank (the sole fuel tank that has a 25-gallon useable capacity). The airplane was recovered from the accident site, and it was transported to a secure location for future examination. The airplane, which was built in 2007, was equipped with a Lycoming O-320-E2A reciprocating engine and a Sensenich Propeller Company 70CM6S16 two-blade fixed pitch aluminum propeller.
On May 28, 2026, about 1440 central daylight time, a Mustang Aeronautics Mustang II airplane, N160MT, sustained substantial damage when it was involved in an accident near Richmond, Texas. The pilot sustained minor injuries. The airplane was operated as a Title 14 Code of Federal Regulations Part 91 personal flight. According to the pilot, he had recently purchased the experimental amateur-built airplane, and the airplane was based at the Covey Trails Airport (X09), Richmond, Texas. The airplane departed from X09 and was performing multiple touch-and-go landings to the single turf runway at the airport. While performing the multiple touch-and-go landings, the pilot reported he was utilizing the carburetor heat. During the final touch-and-go landing, just after the takeoff, the engine sustained a partial loss of power. The engine was unable to provide sufficient power to climb, and the pilot performed a forced landing. The airplane impacted a metal fence, and it came to rest upright on a flat grass field just to the south of X09 near a residential area. The airplane sustained substantial damage to the fuselage and to both wings. The pilot reported that during the recovery of the airplane from the accident site, he drained about 10 gallons of 100 low lead fuel from the fuselage fuel tank (the sole fuel tank that has a 25-gallon useable capacity). The airplane was recovered from the accident site, and it was transported to a secure location for future examination. The airplane, which was built in 2007, was equipped with a Lycoming O-320-E2A reciprocating engine and a Sensenich Propeller Company 70CM6S16 two-blade fixed pitch aluminum propeller.