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.
Iron Mountain, MI
WITNESSES REPORTED SEEING THE AIRPLANE ENTER A SHALLOW LEFT BANK SHORTLY AFTER TAKEOFF. THEY STATED THE BANK GRADUALLY INCREASED TO APPROXIMATELY 60 DEGREES AT WHICH TIME THE NOSE DROPPED AND THE AIRPLANE ENTERED A DESCENDING SPIRAL UNTIL IT CRASHED INTO A RIVER. THE PILOT REPORTED HAVING PROBLEMS WITH THE RUDDER CONTROLS AND AIRSPEED INDICATOR PRIOR TO THE ACCIDENT. THE PILOT MADE SOME ADJUSTMENTS TO THE RUDDER CONTROLS PRIOR TO THIS FLIGHT. POST-ACCIDENT INSPECTION REVEALED DUCT TAPE ON THE FLIGHT CONTROL CABLES. THE RUDDER CONTROL CABLE HAD SLIPPED OFF IT'S PULLEY AND JAMMED BETWEEN THE PULLEY AND THE PULLEY SUPPORT BRACKET.
JAMMING OF THE RUDDER CABLE BETWEEN THE PULLEY AND THE PULLEY SUPPORT BRACKET AND THE PILOT'S CONTINUED OPERATION OF THE AIRPLANE WITH A KNOWN DEFICIENCY.
WITNESSES REPORTED SEEING THE AIRPLANE ENTER A SHALLOW LEFT BANK SHORTLY AFTER TAKEOFF. THEY STATED THE BANK GRADUALLY INCREASED TO APPROXIMATELY 60 DEGREES AT WHICH TIME THE NOSE DROPPED AND THE AIRPLANE ENTERED A DESCENDING SPIRAL UNTIL IT CRASHED INTO A RIVER. THE PILOT REPORTED HAVING PROBLEMS WITH THE RUDDER CONTROLS AND AIRSPEED INDICATOR PRIOR TO THE ACCIDENT. THE PILOT MADE SOME ADJUSTMENTS TO THE RUDDER CONTROLS PRIOR TO THIS FLIGHT. POST-ACCIDENT INSPECTION REVEALED DUCT TAPE ON THE FLIGHT CONTROL CABLES. THE RUDDER CONTROL CABLE HAD SLIPPED OFF IT'S PULLEY AND JAMMED BETWEEN THE PULLEY AND THE PULLEY SUPPORT BRACKET.