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.
Klamath Falls, OR
THE PILOT STATED THAT, DURING TAKEOFF IN A PIPER PA-22 WHICH HAD BEEN CONVERTED TO TAILWHEEL CONFIGURATION, HE WAS HOLDING THE YOKE ALL THE WAY BACK WHILE ADDING POWER. AS THE AIRPLANE'S SPEED INCREASED, THE PILOT MOVED THE YOKE FORWARD TO RAISE THE TAIL. BEFORE THE TAIL ROSE, THE AIRPLANE GROUND LOOPED TO THE LEFT ON THE RUNWAY, CAUSING SUBSTANTIAL DAMAGE. THE PILOT TOLD AN FAA INSPECTOR THAT HE HAD APPLIED FULL RUDDER IN AN ATTEMPT TO PREVENT THE GROUND LOOP.
THE PILOT-IN-COMMAND'S FAILURE TO MAINTAIN DIRECTIONAL CONTROL DURING TAKEOFF, RESULTING IN A GROUND LOOP.
On April 2, 1995, at 1445 hours Pacific daylight time, N8276C, a Piper PA-22 airplane with a tailwheel conversion, ground looped on takeoff in Klamath Falls, Oregon, and was substantially damaged. The private pilot and his three passengers were not injured. Visual meteorological conditions prevailed and a flight plan had been filed. The personal flight was conducted under 14 CFR 91. According to an FAA aviation safety inspector from Hillsboro, Oregon, the pilot stated that he held the control yoke all the way back while adding power for takeoff from runway 13 at the Klamath Falls International Airport. As the speed of the airplane increased, the pilot moved the yoke forward to raise the tail. Before the tail rose, the airplane ground looped to the left. The pilot also stated that he applied full rudder and no brakes in an attempt to prevent the ground loop. The left side of the fuselage and firewall structure were bent. An examination of the airplane by the FAA inspector did not reveal evidence of preimpact mechanical malfunction.