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.
Tallahassee, FL
WHILE CRUISING AT 8000 FEET, THE RIGHT ALTERNATOR LIGHT CAME ON AND THE PILOT ACCOMPLISHED THE REQUIRED PROCEDURES FOR AN ALTERNATOR FAILURE. SHORTLY THEREAFTER, HE NOTICED AN AREA OF DISCOLORATION ON THE INBOARD NACELLE OF THE RIGHT ENGINE AND SAW FLAMES INSIDE THE NACELLE. THE PILOT SECURED THE ENGINE, DECLARED AN EMERGENCY AND MADE A SINGLE ENGINE LANDING AT TALLAHASSEE, FL. EXAMINATION OF THE ENGINE REVEALED A BROKEN TURBOCHARGER EXHAUST CLAMP WHICH ALLOWED THE EXHAUST TUBE TO SEPARATE FROM THE TURBO. HIGH TEMPERATURE EXHAUST GASES THEN STARTED THE FIRE WHICH DISABLED THE ALTERNATOR WIRING. METALLURGICAL EXAMINATION OF THIS CLAMP AND SEVERAL OTHERS THAT HAD FAILED INDICATED THAT THE FAILURES WERE DUE TO HIGH TEMPERATURE EMBRITTLEMENT. THE LACK OF HIGH TEMPERATURE DUCTILITY WAS ATTRIBUTED TO IMPROPER HEAT TREATMENT WHEN THE CLAMPS WERE MANUFACTURED.
WHILE CRUISING AT 8000 FEET, THE RIGHT ALTERNATOR LIGHT CAME ON AND THE PILOT ACCOMPLISHED THE REQUIRED PROCEDURES FOR AN ALTERNATOR FAILURE. SHORTLY THEREAFTER, HE NOTICED AN AREA OF DISCOLORATION ON THE INBOARD NACELLE OF THE RIGHT ENGINE AND SAW FLAMES INSIDE THE NACELLE. THE PILOT SECURED THE ENGINE, DECLARED AN EMERGENCY AND MADE A SINGLE ENGINE LANDING AT TALLAHASSEE, FL. EXAMINATION OF THE ENGINE REVEALED A BROKEN TURBOCHARGER EXHAUST CLAMP WHICH ALLOWED THE EXHAUST TUBE TO SEPARATE FROM THE TURBO. HIGH TEMPERATURE EXHAUST GASES THEN STARTED THE FIRE WHICH DISABLED THE ALTERNATOR WIRING. METALLURGICAL EXAMINATION OF THIS CLAMP AND SEVERAL OTHERS THAT HAD FAILED INDICATED THAT THE FAILURES WERE DUE TO HIGH TEMPERATURE EMBRITTLEMENT. THE LACK OF HIGH TEMPERATURE DUCTILITY WAS ATTRIBUTED TO IMPROPER HEAT TREATMENT WHEN THE CLAMPS WERE MANUFACTURED.