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.
Waxahachie, TX
THE AIRPLANE EXPERIENCED A PARTIAL POWER LOSS, WHILE IN CRUISE FLIGHT AT 2,500 MSL OVER AN AIRPARK. AFTER REDUCING POWER AND APPLYING CARBURETOR HEAT, THE PILOT ATTEMPTED TO EXECUTE A FORCE LANDING TO THE AIRPARK. HOWEVER, SHE OVERSHOT AND LANDED IN A WET PLOWED FIELD BEYOND THE END OF THE RUNWAY. DURING ROLL OUT, THE GEAR DUG INTO THE SOFT TERRAIN AND THE AIRPLANE FLIPPED OVER. EXAMINATION OF THE ENGINE REVEALED THAT A PIECE OF THE #3 EXHAUST VALVE HAD SEPARATED AND HAD BEEN INGESTED. METALLURGICAL EXAMINATION OF THE FAILED VALVE INDICATED THAT IT HAD BEEN EXPOSED TO HIGH TEMPERATURE OPERATION. HOWEVER, THE EXACT ORIGIN OF THE SEPARATION WAS NOT DETERMINED DUE TO MASKING OF THE FRACTURE SURFACES, ACCUMULATION OF EXHAUST DEPOSITS AND POST-SEPARATION MECHANICAL DAMAGE.
FAILURE OF THE #3 EXHAUST VALVE DUE TO EXPOSURE TO OVERTEMPERATURE OPERATING CONDITIONS.
THE AIRPLANE EXPERIENCED A PARTIAL POWER LOSS, WHILE IN CRUISE FLIGHT AT 2,500 MSL OVER AN AIRPARK. AFTER REDUCING POWER AND APPLYING CARBURETOR HEAT, THE PILOT ATTEMPTED TO EXECUTE A FORCE LANDING TO THE AIRPARK. HOWEVER, SHE OVERSHOT AND LANDED IN A WET PLOWED FIELD BEYOND THE END OF THE RUNWAY. DURING ROLL OUT, THE GEAR DUG INTO THE SOFT TERRAIN AND THE AIRPLANE FLIPPED OVER. EXAMINATION OF THE ENGINE REVEALED THAT A PIECE OF THE #3 EXHAUST VALVE HAD SEPARATED AND HAD BEEN INGESTED. METALLURGICAL EXAMINATION OF THE FAILED VALVE INDICATED THAT IT HAD BEEN EXPOSED TO HIGH TEMPERATURE OPERATION. HOWEVER, THE EXACT ORIGIN OF THE SEPARATION WAS NOT DETERMINED DUE TO MASKING OF THE FRACTURE SURFACES, ACCUMULATION OF EXHAUST DEPOSITS AND POST-SEPARATION MECHANICAL DAMAGE.