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.
Truckee, CA
BEFORE THE FLT, THE PLT WAS OBSERVED SCRAPING ICE FROM THE WINGS OF THE ACFT. THE ENG STARTED WITHOUT DIFFICULTY & THE PLT TAXIED TO RWY 28 TO TAKEOFF AT NGT. DURING THE INITIAL CLIMB, THE ACFT ENTERED A LEFT TURN AFTER PASSING THE END OF THE RWY. SUDDENLY, IT ENTERED A DESCENT & CRASHED ON SNOW COVERED TERRAIN. IMPACT OCCURRED ON A HDG OF 140 DEG. THE LEADING EDGES OF BOTH WINGS WERE FLATTENED AGAINST THE MAIN SPAR & THE FUSELAGE FORWARD OF THE EMPENNAGE WAS BUCKLED. A WITNESS STATED THAT THE ENG 'STALLED' BEFORE THE ACFT STARTED A DESCENT. A TEST OF THE FUEL INJECTOR REVEALED IT HAD AN INTERIOR LEAK AROUND THE MIXTURE CONTROL BUSHING SEAL, WHICH ALLOWED UNMETERED FUEL TO ENTER THE ENG. NO OTHER MECHANICAL PART FAILURE/MALFUNCTION WAS FOUND. THE ARPT ELEV WAS 5900'. TWO ACQUAINTANCES OF THE PLT SAID HE RPRTD A FUEL INJECTOR PROBLEM OR A FUEL MIXTURE PROBLEM.
THE PILOT'S DECISION TO FLY WITH A KNOWN DEFICIENCY OF THE AIRCRAFT, THE WORN FUEL INJECTOR WITH AN INTERIOR LEAK, WHICH RESULTED IN LOSS OF ENGINE POWER, AND THE PILOT'S FAILURE TO MAINTAIN ADEQUATE AIRSPEED, WHICH RESULTED IN A STALL.
BEFORE THE FLT, THE PLT WAS OBSERVED SCRAPING ICE FROM THE WINGS OF THE ACFT. THE ENG STARTED WITHOUT DIFFICULTY & THE PLT TAXIED TO RWY 28 TO TAKEOFF AT NGT. DURING THE INITIAL CLIMB, THE ACFT ENTERED A LEFT TURN AFTER PASSING THE END OF THE RWY. SUDDENLY, IT ENTERED A DESCENT & CRASHED ON SNOW COVERED TERRAIN. IMPACT OCCURRED ON A HDG OF 140 DEG. THE LEADING EDGES OF BOTH WINGS WERE FLATTENED AGAINST THE MAIN SPAR & THE FUSELAGE FORWARD OF THE EMPENNAGE WAS BUCKLED. A WITNESS STATED THAT THE ENG 'STALLED' BEFORE THE ACFT STARTED A DESCENT. A TEST OF THE FUEL INJECTOR REVEALED IT HAD AN INTERIOR LEAK AROUND THE MIXTURE CONTROL BUSHING SEAL, WHICH ALLOWED UNMETERED FUEL TO ENTER THE ENG. NO OTHER MECHANICAL PART FAILURE/MALFUNCTION WAS FOUND. THE ARPT ELEV WAS 5900'. TWO ACQUAINTANCES OF THE PLT SAID HE RPRTD A FUEL INJECTOR PROBLEM OR A FUEL MIXTURE PROBLEM.