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.
Smithville, TX
DURING CRUISE AT 8,500 FT MSL THE ENG QUIT. A NIGHT EMERGENCY LANDING WAS MADE AT AN ARPT THAT THE ACFT HAD JUST FLOWN OVER. ON FINAL APPROACH THE PLT COULD NOT SEE THRU THE WINDSHIELD VERY WELL DUE TO OIL BUILDING UP ON THE WINDSHIELD. THE PLT HELD THE GEAR UP UNTIL A LANDING ON THE RWY WAS ASSURED. AFTER CROSSING A ROAD IN FRONT OF THE RWY THE PLT STARTED THE GEAR DOWN. THERE WAS INSUFFICIENT TIME FOR THE RIGHT MAIN LANDING GEAR & NOSE GEAR TO LOCK IN THE DOWN POSITION. THE ACFT TOUCHED DOWN 366 FT BEYOND THE THRESHOLD. ENG TEARDOWN & METALLURGICAL EXAMINATION REVEALED THAT THE #4 CONNECTING ROD HAD FAILED DUE TO FATIGUE. SEM VIEWING OF THE ORIGIN AREA REVEALED A SINGLE FATIGUE INITIATION SITE AT A CHANGE IN CONTOUR ON THE FLANGE END. THE IRREGULAR CONTOUR WAS NOT FOUND AT THE OTHER 3 FLANGE ENDS. ALSO, OXIDE INCLUSIONS & FORGING DEFECTS WERE FOUND ALONG THE ORIGINAL ROD SURFACE.
DURING CRUISE AT 8,500 FT MSL THE ENG QUIT. A NIGHT EMERGENCY LANDING WAS MADE AT AN ARPT THAT THE ACFT HAD JUST FLOWN OVER. ON FINAL APPROACH THE PLT COULD NOT SEE THRU THE WINDSHIELD VERY WELL DUE TO OIL BUILDING UP ON THE WINDSHIELD. THE PLT HELD THE GEAR UP UNTIL A LANDING ON THE RWY WAS ASSURED. AFTER CROSSING A ROAD IN FRONT OF THE RWY THE PLT STARTED THE GEAR DOWN. THERE WAS INSUFFICIENT TIME FOR THE RIGHT MAIN LANDING GEAR & NOSE GEAR TO LOCK IN THE DOWN POSITION. THE ACFT TOUCHED DOWN 366 FT BEYOND THE THRESHOLD. ENG TEARDOWN & METALLURGICAL EXAMINATION REVEALED THAT THE #4 CONNECTING ROD HAD FAILED DUE TO FATIGUE. SEM VIEWING OF THE ORIGIN AREA REVEALED A SINGLE FATIGUE INITIATION SITE AT A CHANGE IN CONTOUR ON THE FLANGE END. THE IRREGULAR CONTOUR WAS NOT FOUND AT THE OTHER 3 FLANGE ENDS. ALSO, OXIDE INCLUSIONS & FORGING DEFECTS WERE FOUND ALONG THE ORIGINAL ROD SURFACE.