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.
Mammoth Lakes, CA
DURING A PLEASURE FLIGHT, JUST AFTER TAKE-OFF, THE ENGINE EXPERIENCED A PARTIAL LOSS OF POWER WHEN THE PLT POSITIONED THE CARB HEAT CONTROL TO FULL COLD. THE PLT STATED THAT IN ORDER TO OBTAIN FULL POWER, DURING THE RUNUP HE WOULD POSITION THE CARB HEAT TO ONE EIGHTH HOT. INSPECTION AND A FLOW TEST OF THE CARB REVEALED THAT THE CARB WOULD SUSTAIN ENGINE OPERATION. THERE WERE NO MECHANICAL FAILURES OR MALFUNCTIONS REPORTED. THE TEMPERATURE RECORDED AT MAMMOTH LAKES AIRPORT 13 MINUTES AFTER THE ACCIDENT WAS 82 DEGREES. THE DENSITY ALTITUDE WAS 10,300 FEET. THE DEW POINT WAS NOT RECORDED THEREFORE THE PROBABILITY OF CARBURETOR ICING COULD NOT BE DETERMINED.
DURING A PLEASURE FLIGHT, JUST AFTER TAKE-OFF, THE ENGINE EXPERIENCED A PARTIAL LOSS OF POWER WHEN THE PLT POSITIONED THE CARB HEAT CONTROL TO FULL COLD. THE PLT STATED THAT IN ORDER TO OBTAIN FULL POWER, DURING THE RUNUP HE WOULD POSITION THE CARB HEAT TO ONE EIGHTH HOT. INSPECTION AND A FLOW TEST OF THE CARB REVEALED THAT THE CARB WOULD SUSTAIN ENGINE OPERATION. THERE WERE NO MECHANICAL FAILURES OR MALFUNCTIONS REPORTED. THE TEMPERATURE RECORDED AT MAMMOTH LAKES AIRPORT 13 MINUTES AFTER THE ACCIDENT WAS 82 DEGREES. THE DENSITY ALTITUDE WAS 10,300 FEET. THE DEW POINT WAS NOT RECORDED THEREFORE THE PROBABILITY OF CARBURETOR ICING COULD NOT BE DETERMINED.