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.
Torrance, CA
THE PLT STATED THAT WHEN HE REACHED APRX 60 FT AGL DURING TAKEOFF, HE NOTICED THE AIRSPEED INDICATOR DROP BELOW 40 MPH. HE SAID THE ENG SOUNDED NORMAL. HE LOWERED THE NOSE OF THE ACFT, BUT THE AIRSPEED INDICATOR READING REMAINED BELOW 40 MPH, SO HE ELECTED TO ABORT. DURING THE ABORT, THE ACFT TOUCHED DOWN 600 FT BEYOND THE END OF THE 5000 FT RWY. AFTER THE 1ST TOUCHDOWN, IT BOUNCED, TRAVEL 170 FT BEFORE THE 2ND TOUCHDOWN, BOUNCED AGAIN & TRAVELED ANOTHER 65 FT BEFORE THE 3RD TOUCHDOWN. IT THEN COLLIDED WITH A BERM & A CHAIN LINK FENCE & TRAVELED AN ADDITIONAL 320 FT BEFORE COMING TO REST. ALL 3 GEAR SEPARATED & THERE WAS EXTENSIVE DAMAGE TO THE NOSE SECTION, BELLY, RIGHT WING & FUSELAGE. BOTH PROPELLER BLADES WERE CURLED REARWARD & EXHIBITED CONSIDERABLE TWISTING, BENDING. EDGE GOUGING & CHORDWISE SCRATCHING. THE PITOT SYS WAS CHECKED, BUT NO SYS LEAKS WERE FOUND & THE AIRSPEED INDICATOR CHECKED WITHIN 1 MPH OF COMPARATOR INDICATIONS.
THE PLT STATED THAT WHEN HE REACHED APRX 60 FT AGL DURING TAKEOFF, HE NOTICED THE AIRSPEED INDICATOR DROP BELOW 40 MPH. HE SAID THE ENG SOUNDED NORMAL. HE LOWERED THE NOSE OF THE ACFT, BUT THE AIRSPEED INDICATOR READING REMAINED BELOW 40 MPH, SO HE ELECTED TO ABORT. DURING THE ABORT, THE ACFT TOUCHED DOWN 600 FT BEYOND THE END OF THE 5000 FT RWY. AFTER THE 1ST TOUCHDOWN, IT BOUNCED, TRAVEL 170 FT BEFORE THE 2ND TOUCHDOWN, BOUNCED AGAIN & TRAVELED ANOTHER 65 FT BEFORE THE 3RD TOUCHDOWN. IT THEN COLLIDED WITH A BERM & A CHAIN LINK FENCE & TRAVELED AN ADDITIONAL 320 FT BEFORE COMING TO REST. ALL 3 GEAR SEPARATED & THERE WAS EXTENSIVE DAMAGE TO THE NOSE SECTION, BELLY, RIGHT WING & FUSELAGE. BOTH PROPELLER BLADES WERE CURLED REARWARD & EXHIBITED CONSIDERABLE TWISTING, BENDING. EDGE GOUGING & CHORDWISE SCRATCHING. THE PITOT SYS WAS CHECKED, BUT NO SYS LEAKS WERE FOUND & THE AIRSPEED INDICATOR CHECKED WITHIN 1 MPH OF COMPARATOR INDICATIONS.