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.
Fort Wayne, IN
WHEN A DESCENT WAS COMMENCED FROM 11,000 FEET, MULTIPLE STATIC DISCHARGES OCCURRED ON BOTH THE CAPTAIN'S AND FIRST OFFICER'S WINDSHIELDS, FOLLOWED BY LOSS OF BOTH THE CAPTAIN'S AND FIRST OFFICER'S EFIS DISPLAYS. THE FLIGHT WAS CONTINUED TO THE DESTINATION ON PRIMARY FLIGHT DISPLAYS. ENROUTE A RIGHT ENGINE FIRE WARNING INDICATION WAS RECEIVED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT AND A SUBSEQUENT EXAMINATION REVEALED THAT 24 STATIC DISCHARGE WICKS WERE FOUND TO BE DEFECTIVE. SEVERAL STATIC WICKS WERE NOT BONDED TO THE AIRFRAME. OTHER SIMILAR BONDING PROBLEMS WERE FOUND ON THE AIRPLANE. THE FAILURE OF THE ENGINE FIRE WARNING SYSTEM WAS TRACED TO A CONTAMINATED ELECTRICAL CONNECTOR.
FAILURE OF COMPANY MAINTENANCE PERSONNEL TO MAINTAIN THE AIRPLANE IN ACCORDANCE WITH EXISTING SERVICE BULLETINS.
WHEN A DESCENT WAS COMMENCED FROM 11,000 FEET, MULTIPLE STATIC DISCHARGES OCCURRED ON BOTH THE CAPTAIN'S AND FIRST OFFICER'S WINDSHIELDS, FOLLOWED BY LOSS OF BOTH THE CAPTAIN'S AND FIRST OFFICER'S EFIS DISPLAYS. THE FLIGHT WAS CONTINUED TO THE DESTINATION ON PRIMARY FLIGHT DISPLAYS. ENROUTE A RIGHT ENGINE FIRE WARNING INDICATION WAS RECEIVED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT AND A SUBSEQUENT EXAMINATION REVEALED THAT 24 STATIC DISCHARGE WICKS WERE FOUND TO BE DEFECTIVE. SEVERAL STATIC WICKS WERE NOT BONDED TO THE AIRFRAME. OTHER SIMILAR BONDING PROBLEMS WERE FOUND ON THE AIRPLANE. THE FAILURE OF THE ENGINE FIRE WARNING SYSTEM WAS TRACED TO A CONTAMINATED ELECTRICAL CONNECTOR.