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.
Oshtemo, MI
WHILE EN ROUTE BACK TO THE AIRSTRIP AFTER A LOCAL FLIGHT A LOSS OF ENGINE POWER WAS EXPERIENCED. THE PILOT STATED HE APPLIED CARBURETOR HEAT AND ENGINE POWER WAS REGAINED. AFTER REMOVING CARBURETOR HEAT, THE ENGINE RPM AGAIN DECREASED. AFTER THIS OCCURRED TWO MORE TIMES, THE PILOT CHOSE A FIELD IN WHICH TO MAKE AN EMERGENCY LANDING. THE TERRAIN WAS ROUGH AND DURING THE LANDING ROLL, THE RIGHT WING CONTACTED THE GROUND, AND THE NOSE GEAR COLLAPSED. ICING PROBABILITY CHARTS INDICATE THAT THE EXISTING TEMPERATURE/DEWPOINT OF 25 DEGREES AND 16 DEGREES RESPECTIVELY WAS CONDUCIVE TO THE FORMATION OF LIGHT CARBURETOR ICING AT GLIDE AND CRUISE POWER SETTINGS.
IMPROPER USE OF CARBURETOR HEAT BY THE PILOT-IN-COMMAND.
WHILE EN ROUTE BACK TO THE AIRSTRIP AFTER A LOCAL FLIGHT A LOSS OF ENGINE POWER WAS EXPERIENCED. THE PILOT STATED HE APPLIED CARBURETOR HEAT AND ENGINE POWER WAS REGAINED. AFTER REMOVING CARBURETOR HEAT, THE ENGINE RPM AGAIN DECREASED. AFTER THIS OCCURRED TWO MORE TIMES, THE PILOT CHOSE A FIELD IN WHICH TO MAKE AN EMERGENCY LANDING. THE TERRAIN WAS ROUGH AND DURING THE LANDING ROLL, THE RIGHT WING CONTACTED THE GROUND, AND THE NOSE GEAR COLLAPSED. ICING PROBABILITY CHARTS INDICATE THAT THE EXISTING TEMPERATURE/DEWPOINT OF 25 DEGREES AND 16 DEGREES RESPECTIVELY WAS CONDUCIVE TO THE FORMATION OF LIGHT CARBURETOR ICING AT GLIDE AND CRUISE POWER SETTINGS.