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.
Montgomery, AL
DURING INITIAL CLIMB PHASE OF AN EXPERIMENTAL FLT FROM MGM, AL, THE PLT RPTED THAT THE LEFT ENGINE HAD FAILED AND AN ATTEMPT WAS MADE TO FEATHER THE PROP. THE PLT RADIOED DANNELLY TOWER THAT THE ACFT WAS RETURNING TO THE ARPT. THEN THE PLT RPTED THAT THE RIGHT ENGINE LOST THRUST, HOWEVER THE RIGHT PROP WAS NOT FEATHERED BECAUSE HE WAS NOT SURE IF THE ENGINE WAS PRODUCING POWER. A GEAR-UP FORCED LANDING WAS MADE ON A 4-LANE HIGHWAY. THE ACFT ENGINES WERE FUELED WITH ALCOHOL WITH APPROVAL OF THE FAA FOR RESEARCH AND DEVELOPMENT. THREE DAYS PRIOR TO THE ACCIDENT THE ACFT EXPERIENCED POWER SURGES AND MADE A PRECAUTIONARY LANDING. NO PROBLEMS WERE FOUND AND THE FLIGHT WAS CONTINUED. INSPECTION OF THE ACFT REVEALED THE RIGHT PROP FEATHERED AND THE LEFT PROP IN LOW PITCH. THE ACFT WGT AND BAL INDICATED APPROX. 400# OVER GROSS WEIGHT. THE ENGINES WERE SUCCESSFULLY TEST RUN. THERE HAS BEEN NO DETERMINATION AS TO THE CAUSE OF THE RPTED ENGINE FAILURES.
DURING INITIAL CLIMB PHASE OF AN EXPERIMENTAL FLT FROM MGM, AL, THE PLT RPTED THAT THE LEFT ENGINE HAD FAILED AND AN ATTEMPT WAS MADE TO FEATHER THE PROP. THE PLT RADIOED DANNELLY TOWER THAT THE ACFT WAS RETURNING TO THE ARPT. THEN THE PLT RPTED THAT THE RIGHT ENGINE LOST THRUST, HOWEVER THE RIGHT PROP WAS NOT FEATHERED BECAUSE HE WAS NOT SURE IF THE ENGINE WAS PRODUCING POWER. A GEAR-UP FORCED LANDING WAS MADE ON A 4-LANE HIGHWAY. THE ACFT ENGINES WERE FUELED WITH ALCOHOL WITH APPROVAL OF THE FAA FOR RESEARCH AND DEVELOPMENT. THREE DAYS PRIOR TO THE ACCIDENT THE ACFT EXPERIENCED POWER SURGES AND MADE A PRECAUTIONARY LANDING. NO PROBLEMS WERE FOUND AND THE FLIGHT WAS CONTINUED. INSPECTION OF THE ACFT REVEALED THE RIGHT PROP FEATHERED AND THE LEFT PROP IN LOW PITCH. THE ACFT WGT AND BAL INDICATED APPROX. 400# OVER GROSS WEIGHT. THE ENGINES WERE SUCCESSFULLY TEST RUN. THERE HAS BEEN NO DETERMINATION AS TO THE CAUSE OF THE RPTED ENGINE FAILURES.