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.
Boca Raton, FL
THE PILOT STATED THAT DURING A CLIMB AFTER TAKEOFF AT ABOUT 150 FEET, HE HEARD A LOUD BANG FOLLOWED BY A DROP TO 30 PSI ON THE RIGHT ENGINE MANIFOLD PRESSURE GAUGE. WHILE TURNING FOR A LEFT DOWNWIND TO RETURN TO THE AIRPORT, HE SECURED THE RIGHT ENGINE AND MOVED THE LEFT ENGINE THROTTLE AND PROP CONTROL TO MAXIMUM POWER AND RPM. HE STATED THAT HE COULD NOT MAINTAIN ALTITUDE AND SELECTED A FORCE LANDING AREA IN A VACANT FIELD. DURING THE LANDING, THE LEFT WING TANK WAS RUPTURED BY SCRUB BUSHES AND TREES. BOTH ENGINES OPERATED NORMALLY DURING POST-ACCIDENT ENGINE RUNS.
IMPROPER REMEDIAL ACTION BY THE PILOT. A FACTOR RELATED TO THE ACCIDENT WAS: LOSS OF ENGINE POWER IN THE RIGHT ENGINE DUE TO AN UNDETERMINED REASON.
THE PILOT STATED THAT DURING A CLIMB AFTER TAKEOFF AT ABOUT 150 FEET, HE HEARD A LOUD BANG FOLLOWED BY A DROP TO 30 PSI ON THE RIGHT ENGINE MANIFOLD PRESSURE GAUGE. WHILE TURNING FOR A LEFT DOWNWIND TO RETURN TO THE AIRPORT, HE SECURED THE RIGHT ENGINE AND MOVED THE LEFT ENGINE THROTTLE AND PROP CONTROL TO MAXIMUM POWER AND RPM. HE STATED THAT HE COULD NOT MAINTAIN ALTITUDE AND SELECTED A FORCE LANDING AREA IN A VACANT FIELD. DURING THE LANDING, THE LEFT WING TANK WAS RUPTURED BY SCRUB BUSHES AND TREES. BOTH ENGINES OPERATED NORMALLY DURING POST-ACCIDENT ENGINE RUNS.