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.
Newnan, GA
DURING THE INITIAL CLIMB AFTER TAKE OFF, WITNESSES NOTED THAT THE ENGINE ON THE MOTORIZED GLIDER HAD QUIT OR WAS SPUTTERING. THE GLIDER PASSED OVER TWO ADDITIONAL WITNESSES, JUST ABOVE THE TREE TOPS, WITH THE PROPELLER WINDMILLING. THE ENGINE WAS AGAIN HEARD BUT WAS DESCRIBED AS TOO LOUD & RACING. AFTERWARDS THE SOUND OF AN IMPACT WAS HEARD. AN EXAMINATION OF THE ENGINE FAILED TO REVEAL AN EXPLANATION FOR THE LOSS OF ENGINE POWER. THE FLIGHT CONTROLS WERE FOUND INTACT & FUNCTIONAL. AN EXAMINATION OF THE ACCIDENT SITE INDICATED THAT THE GLIDER HAD IMPACTED IN A NEARLY VERTICAL NOSE DOWN ATTITUDE. IT CRASHED IN AN OPEN FIELD JUST AFTER OVERFLYING THE EDGE OF THE TREE LINE WHICH BORDERED THE OPEN FIELD.
THE LOSS OF ENGINE POWER FOR UNDETERMINED REASONS, AND THE PILOT'S FAILURE TO MAINTAIN AIRSPEED, WHICH RESULTED IN AN INADVERTENT STALL AT TOO LOW OF AN ALTITUDE TO EFFECT RECOVERY.
DURING THE INITIAL CLIMB AFTER TAKE OFF, WITNESSES NOTED THAT THE ENGINE ON THE MOTORIZED GLIDER HAD QUIT OR WAS SPUTTERING. THE GLIDER PASSED OVER TWO ADDITIONAL WITNESSES, JUST ABOVE THE TREE TOPS, WITH THE PROPELLER WINDMILLING. THE ENGINE WAS AGAIN HEARD BUT WAS DESCRIBED AS TOO LOUD & RACING. AFTERWARDS THE SOUND OF AN IMPACT WAS HEARD. AN EXAMINATION OF THE ENGINE FAILED TO REVEAL AN EXPLANATION FOR THE LOSS OF ENGINE POWER. THE FLIGHT CONTROLS WERE FOUND INTACT & FUNCTIONAL. AN EXAMINATION OF THE ACCIDENT SITE INDICATED THAT THE GLIDER HAD IMPACTED IN A NEARLY VERTICAL NOSE DOWN ATTITUDE. IT CRASHED IN AN OPEN FIELD JUST AFTER OVERFLYING THE EDGE OF THE TREE LINE WHICH BORDERED THE OPEN FIELD.