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.
Castroville, CA
THE ACFT LANDED HARD AND ROLLED OVER AFTER THE LNDG SKID FAILED IN A FORCED LNDG. THE PLT SAID HE WAS CRUSING AT 500 FT AGL OVER AN OPEN FIELD WHEN HE HEARD A LOUD BANG. THE HELICOPTER BEGAN TO VIBRATE SEVERELY AND SPIRAL TO THE RIGHT. THE PLT LOST GROUND REFERENCE IN THE PRE-DAWN DARKNESS WHEN HE TURNED ON THE LIGHTS. NOT WANTING TO LAND TOO HARD HE ELECTED TO LEAVE THE ENG RUNNING AND NOT AUTO-ROTATE. INVESTIGATION INDICATED THAT ONE TAIL ROTOR BLADE HAD SEPARATED AT THE TENSION TORSION STRAP ATTACH BOLT HOLE. THIS IS THE TRANSITION AREA WHERE THE BLADE ROOT CASTING AND SHEET METAL BLADE SKIN ARE JOINED. THE FRACTURE SURFACE OF THE CASTING APPEARED TO BE OVERLOADED WITH NO APPARENT INDICATION OF FATIGUE. THE OUTBOARD BLADE SECTION SHOWED NO INDICATION OF FOREIGN OBJECT CONTACT. ALL COMPONENTS OF THE HELICOPTER WERE LOCATED IN THE IMPACT AREA EXCEPT ONE TAIL ROTOR BLADE.
THE ACFT LANDED HARD AND ROLLED OVER AFTER THE LNDG SKID FAILED IN A FORCED LNDG. THE PLT SAID HE WAS CRUSING AT 500 FT AGL OVER AN OPEN FIELD WHEN HE HEARD A LOUD BANG. THE HELICOPTER BEGAN TO VIBRATE SEVERELY AND SPIRAL TO THE RIGHT. THE PLT LOST GROUND REFERENCE IN THE PRE-DAWN DARKNESS WHEN HE TURNED ON THE LIGHTS. NOT WANTING TO LAND TOO HARD HE ELECTED TO LEAVE THE ENG RUNNING AND NOT AUTO-ROTATE. INVESTIGATION INDICATED THAT ONE TAIL ROTOR BLADE HAD SEPARATED AT THE TENSION TORSION STRAP ATTACH BOLT HOLE. THIS IS THE TRANSITION AREA WHERE THE BLADE ROOT CASTING AND SHEET METAL BLADE SKIN ARE JOINED. THE FRACTURE SURFACE OF THE CASTING APPEARED TO BE OVERLOADED WITH NO APPARENT INDICATION OF FATIGUE. THE OUTBOARD BLADE SECTION SHOWED NO INDICATION OF FOREIGN OBJECT CONTACT. ALL COMPONENTS OF THE HELICOPTER WERE LOCATED IN THE IMPACT AREA EXCEPT ONE TAIL ROTOR BLADE.