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.
El Paso, TX
FIRST EVIDENCE OF LANDING GEAR TIRE MARKS WERE FOUND APRX 4,000 FT DOWN THE RWY, RIGHT OF CENTERLINE AND CONTINUED UNTIL THE ACFT ROLLED OFF THE RIGHT SIDE OF THE RWY. ALL 3 LANDING GEAR COLLAPSED IN THE SOFT DIRT AND GRAVEL. ACCORDING TO THE PLT, WHEN THE AUTO-PILOT WAS DISENGAGED ON FINAL APPROACH, 3 MILES OUT, THE ACFT YAWED RIGHT. POWER AND RUDDER WERE USED TO MAINTAIN CONTROL. AT TOUCHDOWN POWER WAS REDUCED AND SHORTLY THEREAFTER THE ACFT DRIFTED RIGHT DESPITE THE APPLICATION OF LEFT RUDDER AND BRAKE. EXAM OF THE WRECKAGE REVEALED NO MECHANICAL MALFUNCTIONS IN THE AUTO-PILOT, WHEEL BRAKES, FLIGHT CONTROLS, AND TRIM SYSTEMS. THE CAUSE OF THE DIRECTIONAL CONTROL LOSS WAS NOT DETERMINED.
FIRST EVIDENCE OF LANDING GEAR TIRE MARKS WERE FOUND APRX 4,000 FT DOWN THE RWY, RIGHT OF CENTERLINE AND CONTINUED UNTIL THE ACFT ROLLED OFF THE RIGHT SIDE OF THE RWY. ALL 3 LANDING GEAR COLLAPSED IN THE SOFT DIRT AND GRAVEL. ACCORDING TO THE PLT, WHEN THE AUTO-PILOT WAS DISENGAGED ON FINAL APPROACH, 3 MILES OUT, THE ACFT YAWED RIGHT. POWER AND RUDDER WERE USED TO MAINTAIN CONTROL. AT TOUCHDOWN POWER WAS REDUCED AND SHORTLY THEREAFTER THE ACFT DRIFTED RIGHT DESPITE THE APPLICATION OF LEFT RUDDER AND BRAKE. EXAM OF THE WRECKAGE REVEALED NO MECHANICAL MALFUNCTIONS IN THE AUTO-PILOT, WHEEL BRAKES, FLIGHT CONTROLS, AND TRIM SYSTEMS. THE CAUSE OF THE DIRECTIONAL CONTROL LOSS WAS NOT DETERMINED.