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.
Shaftsbury, VT
THE LAKE AMPHIBIAN WAS BEING FLOWN WITH TWO FERRY TANKS INSTALLED IN THE CABIN. THE PILOT DEPARTED WITH FULL FUEL IN THE AIRCRAFT TANKS AND 15 GALLONS IN THE FERRY TANKS. THE CENTER OF GRAVITY AT ZERO FUEL WEIGHT WAS 3/4 INCH PAST THE AFT LIMIT. WITH ADDITION OF FUEL THE POSITION OF THE CG REMAINED UNCHANGED, HOWEVER, THE AFT LIMIT OF THE ENVELOPE MOVED FORWARD WITH HIGHER WEIGHTS. A CONNECTION WHERE THE FERRY TANKS WERE PLUMBED INTO THE AIRCRAFT SYSTEM LEAKED AND ALLOWED AIR TO BE SUCKED INTO THE SYSTEM. WITNESSES REPORTED THE ENGINE INTERMITTENT, THEN THE AIRCRAFT ENTERED A SPIN FROM WHICH IT DID NOT RECOVER.
THE LAKE AMPHIBIAN WAS BEING FLOWN WITH TWO FERRY TANKS INSTALLED IN THE CABIN. THE PILOT DEPARTED WITH FULL FUEL IN THE AIRCRAFT TANKS AND 15 GALLONS IN THE FERRY TANKS. THE CENTER OF GRAVITY AT ZERO FUEL WEIGHT WAS 3/4 INCH PAST THE AFT LIMIT. WITH ADDITION OF FUEL THE POSITION OF THE CG REMAINED UNCHANGED, HOWEVER, THE AFT LIMIT OF THE ENVELOPE MOVED FORWARD WITH HIGHER WEIGHTS. A CONNECTION WHERE THE FERRY TANKS WERE PLUMBED INTO THE AIRCRAFT SYSTEM LEAKED AND ALLOWED AIR TO BE SUCKED INTO THE SYSTEM. WITNESSES REPORTED THE ENGINE INTERMITTENT, THEN THE AIRCRAFT ENTERED A SPIN FROM WHICH IT DID NOT RECOVER.