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.
Friendly, MD
SHORTLY AFTER TAKEOFF AT AN ALTITUDE OF 200 FT AGL, A POWER LOSS WAS EXPERIENCED ON THE LEFT ENGINE. ACCORDING TO THE PLT, WHEN THE THROTTLE WAS RETARDED TO VERIFY THE ENGINE FAILURE, THE ENGINE SEEMED TO 'COME BACK TO LIFE'. THE THROTTLE WAS ADVANCED AND ONCE AGAIN A LOSS OF POWER WAS EXPERIENCED. UNABLE TO GAIN ENOUGH ALTITUDE TO CLEAR THE SURROUNDING TERRAIN AND RETURN TO THE AIRPORT, THE PLT ELECTED TO MAKE A GEAR-UP FORCED LANDING IN A FIELD. THE AIRPLANE SLID FOR 333 FT BEFORE COMING TO REST. INSPECTION OF THE AIRPLANE, ENGINE AND ENGINE COMPONENTS FAILED TO REVEAL ANY MECHANICAL FAILURE/MALFUNCTION. THE ONLY DISCREPANCY FOUND WERE SEVERAL PIECES OF A SILICON RUBBER TYPE MATERIAL INSIDE THE LEFT MAIN FUEL TANK NEAR THE FUEL PICK-UP LINE SCREEN.
SHORTLY AFTER TAKEOFF AT AN ALTITUDE OF 200 FT AGL, A POWER LOSS WAS EXPERIENCED ON THE LEFT ENGINE. ACCORDING TO THE PLT, WHEN THE THROTTLE WAS RETARDED TO VERIFY THE ENGINE FAILURE, THE ENGINE SEEMED TO 'COME BACK TO LIFE'. THE THROTTLE WAS ADVANCED AND ONCE AGAIN A LOSS OF POWER WAS EXPERIENCED. UNABLE TO GAIN ENOUGH ALTITUDE TO CLEAR THE SURROUNDING TERRAIN AND RETURN TO THE AIRPORT, THE PLT ELECTED TO MAKE A GEAR-UP FORCED LANDING IN A FIELD. THE AIRPLANE SLID FOR 333 FT BEFORE COMING TO REST. INSPECTION OF THE AIRPLANE, ENGINE AND ENGINE COMPONENTS FAILED TO REVEAL ANY MECHANICAL FAILURE/MALFUNCTION. THE ONLY DISCREPANCY FOUND WERE SEVERAL PIECES OF A SILICON RUBBER TYPE MATERIAL INSIDE THE LEFT MAIN FUEL TANK NEAR THE FUEL PICK-UP LINE SCREEN.