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.
Santa Ana, CA
THE PILOT REPORTED THAT THE ENGINE LOST POWER AFTER HE HAD RAISED THE GEAR DURING TAKEOFF. HE LOWERED THE NOSE TO AVOID A STALL AND LANDED GEAR-UP AT AND OFF THE END OF THE RUNWAY. REPORTEDLY, TOWER PERSONNEL OBSERVED BLACK SMOKE TRAILING FROM THE BOTTOM OF THE ENGINE COWLING. THE FRONT SEAT PASSENGER, A RATED PILOT, REPORTED THAT THE FUEL PRESSURE NEEDLE WAS PEGGED TO THE HIGH LIMIT. THE PILOT REPORTED THAT THE FUEL FLOW NEEDLE HAD GONE FROM THE 6 O'CLOCK POSITION (36 GPH) TO ABOUT THE 10 TO 11 O'CLOCK POSITION. THERE WAS A HISTORY OF FUEL PRESSURE DISCREPANCIES. THREE FUEL PUMP REPLACEMENTS WERE DOCUMENTED IN THE AIRCRAFT LOGBOOKS. A CHECK OF THE FUEL PUMP REVEALED DISCREPANCIES IN THE FUEL PRESSURE AND FUEL FLOW, BUT THESE INVOLVED LOW OUTPUT RATHER THAN HIGH OUTPUT.
THE PILOT REPORTED THAT THE ENGINE LOST POWER AFTER HE HAD RAISED THE GEAR DURING TAKEOFF. HE LOWERED THE NOSE TO AVOID A STALL AND LANDED GEAR-UP AT AND OFF THE END OF THE RUNWAY. REPORTEDLY, TOWER PERSONNEL OBSERVED BLACK SMOKE TRAILING FROM THE BOTTOM OF THE ENGINE COWLING. THE FRONT SEAT PASSENGER, A RATED PILOT, REPORTED THAT THE FUEL PRESSURE NEEDLE WAS PEGGED TO THE HIGH LIMIT. THE PILOT REPORTED THAT THE FUEL FLOW NEEDLE HAD GONE FROM THE 6 O'CLOCK POSITION (36 GPH) TO ABOUT THE 10 TO 11 O'CLOCK POSITION. THERE WAS A HISTORY OF FUEL PRESSURE DISCREPANCIES. THREE FUEL PUMP REPLACEMENTS WERE DOCUMENTED IN THE AIRCRAFT LOGBOOKS. A CHECK OF THE FUEL PUMP REVEALED DISCREPANCIES IN THE FUEL PRESSURE AND FUEL FLOW, BUT THESE INVOLVED LOW OUTPUT RATHER THAN HIGH OUTPUT.