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.
Miami, FL
ACCORDING TO THE FLIGHT CREW, A LOUD EXPLOSION WAS HEARD A FEW SECONDS AFTER REACHING TAKEOFF POWER AND THE TAKEOFF WAS ABORTED. WHILE TAXIING, THE TOWER INFORMED THE FLIGHT CREW THAT FLAMES WERE COMING FROM THE NO. 4 ENGINE. THE AIRCREW STOPPED THE AIRCRAFT AND COMPLETED THE ENGINE FIRE PROCEDURES; HOWEVER, THE AIRPORT FIRE FIGHTERS EXTINGUISHED THE FIRE. AN INVESTIGATION REVEALED THAT THE NO. 4 ENGINE HAD FAILED AND HIGH ENERGY ENGINE PARTS WERE RELEASED WHICH RESULTED IN DAMAGE TO THE AIRFRAME AND THE NO. 3 ENGINE. MOST OF THE ROTATING COMPONENTS, FORWARD OF 7TH STAGE COMPRESSOR DISK ASSEMBLY, WERE RELEASED DURING THE EXPLOSIVE FAILURE. AN EXAMINATION OF THE FIRST STAGE COMPRESSOR FAN BLADES SHOWED THAT THE NO. 15 FIRST STAGE FAN BLADE, PN 531601K, HAD FAILED FROM FATIGUE. THE FAILURE OCCURRED 3.2 HRS AFTER OVERHAUL.
ACCORDING TO THE FLIGHT CREW, A LOUD EXPLOSION WAS HEARD A FEW SECONDS AFTER REACHING TAKEOFF POWER AND THE TAKEOFF WAS ABORTED. WHILE TAXIING, THE TOWER INFORMED THE FLIGHT CREW THAT FLAMES WERE COMING FROM THE NO. 4 ENGINE. THE AIRCREW STOPPED THE AIRCRAFT AND COMPLETED THE ENGINE FIRE PROCEDURES; HOWEVER, THE AIRPORT FIRE FIGHTERS EXTINGUISHED THE FIRE. AN INVESTIGATION REVEALED THAT THE NO. 4 ENGINE HAD FAILED AND HIGH ENERGY ENGINE PARTS WERE RELEASED WHICH RESULTED IN DAMAGE TO THE AIRFRAME AND THE NO. 3 ENGINE. MOST OF THE ROTATING COMPONENTS, FORWARD OF 7TH STAGE COMPRESSOR DISK ASSEMBLY, WERE RELEASED DURING THE EXPLOSIVE FAILURE. AN EXAMINATION OF THE FIRST STAGE COMPRESSOR FAN BLADES SHOWED THAT THE NO. 15 FIRST STAGE FAN BLADE, PN 531601K, HAD FAILED FROM FATIGUE. THE FAILURE OCCURRED 3.2 HRS AFTER OVERHAUL.