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.
Chena Hot Sprng, AK
THE SIGHTSEEING FLIGHT, CONDUCTED UNDER 14 CFR PART 91, CRASHED ON LANDING. WITNESSES REPORTED THAT THE UPON MAKING INITIAL CONTACT WITH THE SNOW COVERED SURFACE, THE AIRPLANE BOUNCED BACK INTO THE AIR TO A HEIGHT OF TWO TO THREE FEET AND THE RIGHT SKI SEPARATED FROM THE LANDING GEAR STRUCTURE. POST ACCIDENT EXAMINATION DISCLOSED THAT THE FRACTURE OCCURRED AT THE TUBULAR AXLE FLANGE OF THE LANDING GEAR. AN EXAMINATION OF THE FRACTURE REVEALED THAT THERE WERE SEVERAL AREAS AT THE 12 AND 6 O'CLOCK POSITION OF THE FRACTURE SURFACE THAT WERE VERY BRIGHT AND ROUGH. SURFACE AREAS AT THE 3 AND 9 O'CLOCK POSITION WERE DARKER, GRAYISH IN COLOR AND THE SURFACE WAS SOMEWHAT SMOOTHER.
THE TOTAL FAILURE OF THE LANDING GEAR AXLE AS A RESULT OF A PRE EXISTING FRACTURE IN THE AXLE.
THE SIGHTSEEING FLIGHT, CONDUCTED UNDER 14 CFR PART 91, CRASHED ON LANDING. WITNESSES REPORTED THAT THE UPON MAKING INITIAL CONTACT WITH THE SNOW COVERED SURFACE, THE AIRPLANE BOUNCED BACK INTO THE AIR TO A HEIGHT OF TWO TO THREE FEET AND THE RIGHT SKI SEPARATED FROM THE LANDING GEAR STRUCTURE. POST ACCIDENT EXAMINATION DISCLOSED THAT THE FRACTURE OCCURRED AT THE TUBULAR AXLE FLANGE OF THE LANDING GEAR. AN EXAMINATION OF THE FRACTURE REVEALED THAT THERE WERE SEVERAL AREAS AT THE 12 AND 6 O'CLOCK POSITION OF THE FRACTURE SURFACE THAT WERE VERY BRIGHT AND ROUGH. SURFACE AREAS AT THE 3 AND 9 O'CLOCK POSITION WERE DARKER, GRAYISH IN COLOR AND THE SURFACE WAS SOMEWHAT SMOOTHER.