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.
Romulus, MI
THE CAPT MADE A STEEP, SHORT, FAST VISUAL APPROACH TO THE RUNWAY BEHIND A DEPARTING DC-9. THE EVIDENCE INDICATES THE CAPT PLACED THE POWER LEVERS INTO BETA MODE TO SLOW THE AIRCRAFT RAPIDLY AND MAKE A SHORT FIELD LANDING. AN ASYMMETRIC THRUST CONDITION RESULTED. THE AIRCRAFT WAS VERY CLOSE TO THE GROUND AND THE CAPT COULD NOT RECOVER PRIOR TO IMPACT. IMPACT FORCES WERE SURVIVABLE. HOWEVER, THE FATALITIES WERE ATTRIBUTED TO A POSTCRASH FIRE, LACK OF FIRE-BLOCKING MATERIAL, AND POORLY DESIGNED AIRCRAFT COMPONENTS. THE INVESTIGATION REVEALED INCORRECT SPRINGS INSTALLED IN THE PROPELLERS AND HIGHER THAT NORMAL FUEL FLOW SETTINGS. THE EXAMINATION OF THE CERTIFICATION PROCESS INDICATED INEFFECTIVEMANAGEMENT OF BILATERAL TYPE CERTIFICATION BY THE FAA. (FOR FURTHER INFORMATION, SEE NTSB/AAR-88/08.)
THE CAPT MADE A STEEP, SHORT, FAST VISUAL APPROACH TO THE RUNWAY BEHIND A DEPARTING DC-9. THE EVIDENCE INDICATES THE CAPT PLACED THE POWER LEVERS INTO BETA MODE TO SLOW THE AIRCRAFT RAPIDLY AND MAKE A SHORT FIELD LANDING. AN ASYMMETRIC THRUST CONDITION RESULTED. THE AIRCRAFT WAS VERY CLOSE TO THE GROUND AND THE CAPT COULD NOT RECOVER PRIOR TO IMPACT. IMPACT FORCES WERE SURVIVABLE. HOWEVER, THE FATALITIES WERE ATTRIBUTED TO A POSTCRASH FIRE, LACK OF FIRE-BLOCKING MATERIAL, AND POORLY DESIGNED AIRCRAFT COMPONENTS. THE INVESTIGATION REVEALED INCORRECT SPRINGS INSTALLED IN THE PROPELLERS AND HIGHER THAT NORMAL FUEL FLOW SETTINGS. THE EXAMINATION OF THE CERTIFICATION PROCESS INDICATED INEFFECTIVEMANAGEMENT OF BILATERAL TYPE CERTIFICATION BY THE FAA. (FOR FURTHER INFORMATION, SEE NTSB/AAR-88/08.)