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.
Chattanooga, TN
THE ENG LOST POWER PASSING 4,000 FT DURING CLIMBOUT. THE PLT IMMEDIATELY REVERSED COURSE & ATTEMPTED TO REACH LOVELL FIELD. HE WAS UNABLE TO REACH THE RWY & LANDED IN A SHOPPING CENTER PARKING LOT 1 MI SHORT OF THE RWY. THE RIGHT WING STRUCK A SIGNPOST & THE NOSE GR COLLAPSED. THE THROTTLE LINKAGE WAS FOUND SEPARATED AT THE CONTROL SHAFT UNDER THE ROD END THAT CONNECTS TO THE FUEL CONTROL. THE FRACTURE AREA WAS IN THE CONTROL ROD & THE FRACTURE SURFACE EXHIBITED RUST OVER THE ENTIRE BREAK. METALLURGICAL EXAMINATION REVEALED A FATIGUE FRACTURE OF THE CONTROL SHAFT AT THE POINT WHERE THE DRIVE SCREW WAS INSERTED THROUGH THE SLEEVE, THE THREADED BRASS BUSHING & INTO THE CONTROL SHAFT. CESSNA SERVICE BULLETIN 69-16, DATED 7/22/69, IDENTIFIED THIS PROBLEM & DESCRIBED PROCEDURES TO REMEDY THE PROBLEM. SERVICE LETTERS ARENOT MANDATORY & THERE WAS NO RECORD OF COMPLIANCE IN THE ACFT'S LOGBOOK.
THE ENG LOST POWER PASSING 4,000 FT DURING CLIMBOUT. THE PLT IMMEDIATELY REVERSED COURSE & ATTEMPTED TO REACH LOVELL FIELD. HE WAS UNABLE TO REACH THE RWY & LANDED IN A SHOPPING CENTER PARKING LOT 1 MI SHORT OF THE RWY. THE RIGHT WING STRUCK A SIGNPOST & THE NOSE GR COLLAPSED. THE THROTTLE LINKAGE WAS FOUND SEPARATED AT THE CONTROL SHAFT UNDER THE ROD END THAT CONNECTS TO THE FUEL CONTROL. THE FRACTURE AREA WAS IN THE CONTROL ROD & THE FRACTURE SURFACE EXHIBITED RUST OVER THE ENTIRE BREAK. METALLURGICAL EXAMINATION REVEALED A FATIGUE FRACTURE OF THE CONTROL SHAFT AT THE POINT WHERE THE DRIVE SCREW WAS INSERTED THROUGH THE SLEEVE, THE THREADED BRASS BUSHING & INTO THE CONTROL SHAFT. CESSNA SERVICE BULLETIN 69-16, DATED 7/22/69, IDENTIFIED THIS PROBLEM & DESCRIBED PROCEDURES TO REMEDY THE PROBLEM. SERVICE LETTERS ARENOT MANDATORY & THERE WAS NO RECORD OF COMPLIANCE IN THE ACFT'S LOGBOOK.