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.
Conchas Dam, NM
THE AIRPLANE WATERLOOPED DURING THE TAKEOFF RUN AFTER NEARLY WATERLOOPING ON THE PREVIOUS LANDING. POSTACCIDENT EXAMINATION DISCLOSED THE LANDING GEAR CABLE WAS IMPROPERLY RIGGED, ALLOWING THE LEFT AFT PONTOON WHEEL TO DEPLOY. MAXIMUM RPM COULD NOT BE ATTAINED BECAUSE THE PROPELLER GOVERNOR WAS NOT PROPERLY ADJUSTED. A REVIEW OF THE ACCIDENT VIDEO TAPE REVEALED AIRCRAFT HAD ATTAINED SUFFICIENT FLYING SPEED. PILOT DID NOT DEPLOY TAKEOFF FLAPS.
LANDING GEAR LOCKING MECHANISM LOOSE, LANDING GEAR WHEEL DEPLOYED INADVERTENTLY, AND MAINTENANCE ALIGNMENT NOT PERFORMED. FACTORS WERE: PROPELLER GOVERNOR UNDERSPEED, MAINTENANCE ADJUSTMENT NOT CORRECTED, AND LOWERING OF FLAPS NOT PERFORMED.
THE AIRPLANE WATERLOOPED DURING THE TAKEOFF RUN AFTER NEARLY WATERLOOPING ON THE PREVIOUS LANDING. POSTACCIDENT EXAMINATION DISCLOSED THE LANDING GEAR CABLE WAS IMPROPERLY RIGGED, ALLOWING THE LEFT AFT PONTOON WHEEL TO DEPLOY. MAXIMUM RPM COULD NOT BE ATTAINED BECAUSE THE PROPELLER GOVERNOR WAS NOT PROPERLY ADJUSTED. A REVIEW OF THE ACCIDENT VIDEO TAPE REVEALED AIRCRAFT HAD ATTAINED SUFFICIENT FLYING SPEED. PILOT DID NOT DEPLOY TAKEOFF FLAPS.