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.
W Cameron Blk
THE TWIN ENGINE HELICOPTER WAS IN CRUISE FLIGHT OVER THE GULF OF MEXICO, WHEN IT SUDDENLY PITCHED NOSE DOWN AND DESCENDED UNCONTROLLED TO IMPACT INVERTED INTO THE WATER. IT SANK TO A DEPTH OF APPROXIMATELY 380 FEET. AFTER RECOVERY OF THE HELICOPTER, EXAMINATION REVEALED THAT AN INCORRECT HYDRAULIC SWITCH GUARD HELD THE TEST SWITCH IN THE RESET POSITION, ELECTRICALLY ISOLATING HYDRAULIC SYSTEM NUMBER TWO FROM OPERATION, AND THAT THE HYDRAULIC MODULE WAS IN THE NUMBER 1 SYSTEM. FURTHER INSPECTION AND TESTING FOUND A DEFECTIVE MICRO-SWITCH IN THE OUTBOARD LATERAL GUIDE ASSEMBLY OF THE HYDRAULIC MODULE. ADDITIONALLY, THE OPERATOR HAD NOT COMPLIED WITH A REQUIRED SERVICE BULLETIN FOR THE MODULE.
THE PARTIAL ELECTRICAL FAILURE OF THE MICRO-SWITCH FOR THE OUTBOARD LATERAL GUIDE ASSEMBLY, AND THE INCORRECT GUARD INSTALLED ON THE HYDRAULIC TEST SWITCH, RESULTING IN A TOTAL HYDRAULIC FAILURE. FACTORS WERE: THE INCORRECT INSTALLATION OF THE GUARD BY AN UNKNOWN PERSON, THE FAILURE OF THE COMPANY TO COMPLY WITH THE SPECIFIED SERVICE BULLETIN.
THE TWIN ENGINE HELICOPTER WAS IN CRUISE FLIGHT OVER THE GULF OF MEXICO, WHEN IT SUDDENLY PITCHED NOSE DOWN AND DESCENDED UNCONTROLLED TO IMPACT INVERTED INTO THE WATER. IT SANK TO A DEPTH OF APPROXIMATELY 380 FEET. AFTER RECOVERY OF THE HELICOPTER, EXAMINATION REVEALED THAT AN INCORRECT HYDRAULIC SWITCH GUARD HELD THE TEST SWITCH IN THE RESET POSITION, ELECTRICALLY ISOLATING HYDRAULIC SYSTEM NUMBER TWO FROM OPERATION, AND THAT THE HYDRAULIC MODULE WAS IN THE NUMBER 1 SYSTEM. FURTHER INSPECTION AND TESTING FOUND A DEFECTIVE MICRO-SWITCH IN THE OUTBOARD LATERAL GUIDE ASSEMBLY OF THE HYDRAULIC MODULE. ADDITIONALLY, THE OPERATOR HAD NOT COMPLIED WITH A REQUIRED SERVICE BULLETIN FOR THE MODULE.