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.
East Fishkill, NY
After departure, another pilot advised N8511Z that a cowl door was open. The pilot acknowledged, but continued the flight. During the VFR flight, witnesses heard a loud pop and observed the R22 helicopter break apart in flight. One witness observed a light airplane traveling in the opposite direction at the same time. The tail boom was the first piece of the helicopter found along the 584' long wreckage path. The main rotor separated from its drive shaft and there were multiple strikes to the tail boom. Metallurgical examination of the main rotor head components and examination of the engine revealed no evidence of malfunction or failure that could have contributed to the main rotor blade diverging and striking the tail boom, resulting in the in-flight separation of the tail boom. Examination of the right collective control tube revealed a fatigue fracture in the inboard wall of the tube where it is normally lightly loaded. The evidence did not support a conclusion that this was related to loss of main rotor control.
A LOSS OF CONTROL IN FLIGHT FOR UNDETERMINED REASONS.
AFTER DEPARTURE, ANOTHER PILOT ADVISED N8511Z THAT A COWL DOOR WAS OPEN. THE PILOT ACKNOWLEDGED, BUT CONTINUED THE FLIGHT. DURING THE VFR FLIGHT, WITNESSES HEARD A LOUD POP & OBSERVED THE R22 HELICOPTER BREAK APART IN FLIGHT. ONE WITNESS OBSERVED A LIGHT AIRPLANE TRAVELING IN THE OPPOSITE DIRECTION AT THE SAME TIME. THE TAIL BOOM WAS THE FIRST PIECE OF THE HELICOPTER FOUND ALONG THE 584' LONG WRECKAGE PATH. THE MAIN ROTOR SEPARATED FROM ITS DRIVE SHAFT & THERE WERE MULTIPLE STRIKES TO THE TAIL BOOM. METALLURGICAL EXAMINATION OF THE MAIN ROTOR HEAD COMPONENTS & EXAMINATION OF THE ENGINE REVEALED NO EVIDENCE OF MALFUNCTION OR FAILURE THAT COULD HAVE CONTRIBUTED TO THE MAIN ROTOR BLADE DIVERGING & STRIKING THE TAIL BOOM, RESULTING IN THE IN-FLIGHT SEPARATION OF THE TAIL BOOM. EXAMINATION OF THE RIGHT COLLECTIVE CONTROL TUBE REVEALED A FATIGUE FRACTURE IN THE INBOARD WALL OF THE TUBE WHERE IT IS NORMALLY LIGHTLY LOADED. THE EVIDENCE DID NOT SUPPORT A CONCLUSION THAT THIS WAS RELATED TO LOSS OF MAIN ROTOR CONTROL.