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.
Collier Twnshp, PA
DURING ARRIVAL, THE PLT CONTACTED APCH CONTROL & WAS PROVIDED RADAR VECTORS FOR A VISUAL APCH. WHILE ON THE APCH, HE WAS INSTRUCTED TO KEEP HIS SPEED UP UNTIL HE WAS 1 1/2 MI ON FINAL. VECTORS WERE PROVIDE WITH TURNS AS NECESSARY UNTIL THE ACFT WAS 6 1/2 TO 7 MI FROM THE RWY. AT THAT TIME, THE PLT REPORTED THAT HE HAD THE ARPT IN SIGHT. HE WAS THEN INSTRUCTED TO PROCEED INBOUND FOR RWY 32 & TO KEEP HIS SPEED UP AS LONG AS FEASIBLE. THE PLT ACKNOWLEDGED. SHORTLY AFTER THAT, RADIO & RADAR CONTACT WERE LOST. A NUMBER OF WITNESSES HEARD & SAW THE ACFT AT A FASTER THAN NORMAL SPEED. SEVERAL SAW THE ACFT & DEBRIS FALLING AFTER AN IN-FLT BREAKUP OCCURRED. EVIDENCE WAS FOUND THAT THE WINGS & RIGHT HORIZONTAL STABILIZER HAD SEPARATED DOWNWARD & THE LEFT HORIZONTAL STABILIZER HAD SEPARATED UPWARD. THE AILERON, RUDDER & STABILIZER BALANCE WTS WERE STILL IN PLACE. RADAR DATA REVEALED THAT THE GROUND SPEED ON FINAL APCH HAD INCREASED TO 208 KTS. THE NEVER EXCEED SPEED (VNE) WAS 189 KCAS & 197 KIAS. ANOTHER PLT REPORTED LGT TO MOD TURB.
DURING ARRIVAL, THE PLT CONTACTED APCH CONTROL & WAS PROVIDED RADAR VECTORS FOR A VISUAL APCH. WHILE ON THE APCH, HE WAS INSTRUCTED TO KEEP HIS SPEED UP UNTIL HE WAS 1 1/2 MI ON FINAL. VECTORS WERE PROVIDE WITH TURNS AS NECESSARY UNTIL THE ACFT WAS 6 1/2 TO 7 MI FROM THE RWY. AT THAT TIME, THE PLT REPORTED THAT HE HAD THE ARPT IN SIGHT. HE WAS THEN INSTRUCTED TO PROCEED INBOUND FOR RWY 32 & TO KEEP HIS SPEED UP AS LONG AS FEASIBLE. THE PLT ACKNOWLEDGED. SHORTLY AFTER THAT, RADIO & RADAR CONTACT WERE LOST. A NUMBER OF WITNESSES HEARD & SAW THE ACFT AT A FASTER THAN NORMAL SPEED. SEVERAL SAW THE ACFT & DEBRIS FALLING AFTER AN IN-FLT BREAKUP OCCURRED. EVIDENCE WAS FOUND THAT THE WINGS & RIGHT HORIZONTAL STABILIZER HAD SEPARATED DOWNWARD & THE LEFT HORIZONTAL STABILIZER HAD SEPARATED UPWARD. THE AILERON, RUDDER & STABILIZER BALANCE WTS WERE STILL IN PLACE. RADAR DATA REVEALED THAT THE GROUND SPEED ON FINAL APCH HAD INCREASED TO 208 KTS. THE NEVER EXCEED SPEED (VNE) WAS 189 KCAS & 197 KIAS. ANOTHER PLT REPORTED LGT TO MOD TURB.