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.
San Diego, CA
DURING THE INITIAL CLIMB AFTER TAKEOFF, THE ENGINE LOST PARTIAL POWER. A TURN WAS MADE TO LAND ON RWY 10R, BUT THE PILOT WAS UNABLE TO REACH THE LANDING AREA. SUBSEQUENTLY, HE MADE A WHEELS-UP LANDING SHORT OF THE RUNWAY. AN INSPECTIONOF THE ENGINE REVEALED EVIDENCE OF DETONATION OR PREIGNITION IN THE NUMBER FOUR CYLINDER. ANOTHER PILOT, WHO HAD FLOWN THE AIRPLANE ON THE PREVIOUS FLIGHT, SAID THAT WHEN HE WAS RETURNING TO THE AIRPORT FROM A LONG FLIGHT, THE ENGINE BEGAN TO VIBRATE AND THE OIL TEMP AND CYLINDER HEAD TEMP ROSE ABOVE THE RED LINE. AFTER LANDING, HE NOTIFIED THE OPERATOR. THE OPERATOR REPORTED THAT A NEW SET OF SPARK PLUGS WERE INSTALLED AFTER THAT FLIGHT AND THE ENGINE RAN FINE.
DURING THE INITIAL CLIMB AFTER TAKEOFF, THE ENGINE LOST PARTIAL POWER. A TURN WAS MADE TO LAND ON RWY 10R, BUT THE PILOT WAS UNABLE TO REACH THE LANDING AREA. SUBSEQUENTLY, HE MADE A WHEELS-UP LANDING SHORT OF THE RUNWAY. AN INSPECTIONOF THE ENGINE REVEALED EVIDENCE OF DETONATION OR PREIGNITION IN THE NUMBER FOUR CYLINDER. ANOTHER PILOT, WHO HAD FLOWN THE AIRPLANE ON THE PREVIOUS FLIGHT, SAID THAT WHEN HE WAS RETURNING TO THE AIRPORT FROM A LONG FLIGHT, THE ENGINE BEGAN TO VIBRATE AND THE OIL TEMP AND CYLINDER HEAD TEMP ROSE ABOVE THE RED LINE. AFTER LANDING, HE NOTIFIED THE OPERATOR. THE OPERATOR REPORTED THAT A NEW SET OF SPARK PLUGS WERE INSTALLED AFTER THAT FLIGHT AND THE ENGINE RAN FINE.