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.
Henderson, NV
About 100 feet above ground level during initial climb, the experimental airplane's engine began vibrating, sputtering, and losing power. The pilot adjusted the mixture and throttle controls, but was unable to regain sufficient rpm to sustain flight. The pilot made a forced landing on rough desert terrain, about 1 mile from the departure airport. During the subsequent engine examination, no evidence of case or cylinder damage was noted. Oil was found on the dipstick, the carburetor was intact, and the throttle control was secure. The reason for the partial loss of engine power was not determined.
A partial loss of engine power for undetermined nonmechanical reasons. A contributing factor was the rough nature of the terrain used for the forced landing.
On October 2, 1999, about 0845 hours Pacific daylight time, an experimental Ismari Canard C3A, N4526W, owned and operated by the pilot, experienced a partial loss of engine power during initial climb from the Henderson, Nevada, airport. The commercial pilot made a forced landing in rough terrain, and the homebuilt airplane was substantially damaged. The personal flight was conducted under the provisions of 14 CFR Part 91. The pilot was not injured. Visual meteorological conditions prevailed at the time of the local area flight, and no flight plan was filed. The flight, which lasted about 3 minutes, was originating at the time of the accident. The pilot reported that upon climbing 100 feet above ground level the engine began vibrating, sputtering, and losing power. Unable to resolve the problem by adjusting the mixture and throttle controls, and with reduced rpm, the pilot was unable to maintain flight. He made a forced landing in desert terrain, about 1 mile southwest of Henderson. The Federal Aviation Administration (FAA) coordinator performed a visual, external examination of the engine. No evidence of case or cylinder damage was noted. Oil was present on the dipstick, and the carburetor was intact without any apparent damage. The throttle control was found intact.