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.
Rancho Bernardo, CA
ACCORDING TO THE PLT, HE WAS ABOUT 10 FT AGL IN A HOVER, WITH A LEFT QUARTERING TAILWIND AT 5, GUSTING 10 KTS, WHEN HE ATTEMPTED A LEFT PEDAL TURN. HE SAID THE HELICOPTER BEGAN TO TURN TO THE RIGHT & ADDITIONAL LEFT PEDAL APPLICATION HAD NO EFFECT. HE ROLLED THE THROTTLE OFF & ATTEMPTED TO LAND, BUT THE HELICOPTER CONTINUED TURNING TO THE RIGHT & CRASHED. HE REMEMBERED HEARING THE LOW RPM WARNING HORN, BUT DID NOT REMEMBER SEEING THE LOW RPM LIGHT. ALSO, HE DID NOT RECALL HEARING ANY UNUSUAL NOISES OR FEELING ANY UNUSUAL VIBRATIONS BEFORE IMPACT. AN EXAMINATION OF THE HELICOPTER & DAMAGED PARTS WAS MADE, BUT NO PREIMPACT MALFUNCTION OR FAILURE OF THE ENG; AIRFRAME OR FLT CONTROL SYS WAS FOUND.
ACCORDING TO THE PLT, HE WAS ABOUT 10 FT AGL IN A HOVER, WITH A LEFT QUARTERING TAILWIND AT 5, GUSTING 10 KTS, WHEN HE ATTEMPTED A LEFT PEDAL TURN. HE SAID THE HELICOPTER BEGAN TO TURN TO THE RIGHT & ADDITIONAL LEFT PEDAL APPLICATION HAD NO EFFECT. HE ROLLED THE THROTTLE OFF & ATTEMPTED TO LAND, BUT THE HELICOPTER CONTINUED TURNING TO THE RIGHT & CRASHED. HE REMEMBERED HEARING THE LOW RPM WARNING HORN, BUT DID NOT REMEMBER SEEING THE LOW RPM LIGHT. ALSO, HE DID NOT RECALL HEARING ANY UNUSUAL NOISES OR FEELING ANY UNUSUAL VIBRATIONS BEFORE IMPACT. AN EXAMINATION OF THE HELICOPTER & DAMAGED PARTS WAS MADE, BUT NO PREIMPACT MALFUNCTION OR FAILURE OF THE ENG; AIRFRAME OR FLT CONTROL SYS WAS FOUND.