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.
Wichita, KS
AFTER A TOUCH-&-GO LANDING, THE FLT CREW NOTED A PROBLEM WITH THE LANDING GEAR. A CHECK OF THE HYDRAULIC SYS REVEALED A LACK OF FLUID IN THE RESERVOIR; THE PLTS WERE UNABLE TO EITHER RETRACT OR EXTEND THE GEAR. SUBSEQUENTLY, THEY LANDED THE ACFT WITH THE NOSE & RGT MAIN GEAR EXTENDED & THE LEFT MAIN GEAR IN A TRAIL POSITION. THE LEFT WING TIP, LEFT MAIN GEAR DOOR & LEFT STABILIZER WERE DAMAGED DURING THE LANDING. AN EXAM OF THE HYDRAULIC SYS REVEALED THAT A HOSE TO THE RIGHT MAIN GEAR DOOR ACTUATOR WAS LEAKING & HAD PERMITTED DEPLETION OF THE HYDRAULIC FLUID. THE HOSE WAS DETERIORATED FROM AGE.
AFTER A TOUCH-&-GO LANDING, THE FLT CREW NOTED A PROBLEM WITH THE LANDING GEAR. A CHECK OF THE HYDRAULIC SYS REVEALED A LACK OF FLUID IN THE RESERVOIR; THE PLTS WERE UNABLE TO EITHER RETRACT OR EXTEND THE GEAR. SUBSEQUENTLY, THEY LANDED THE ACFT WITH THE NOSE & RGT MAIN GEAR EXTENDED & THE LEFT MAIN GEAR IN A TRAIL POSITION. THE LEFT WING TIP, LEFT MAIN GEAR DOOR & LEFT STABILIZER WERE DAMAGED DURING THE LANDING. AN EXAM OF THE HYDRAULIC SYS REVEALED THAT A HOSE TO THE RIGHT MAIN GEAR DOOR ACTUATOR WAS LEAKING & HAD PERMITTED DEPLETION OF THE HYDRAULIC FLUID. THE HOSE WAS DETERIORATED FROM AGE.