EASA AD US-2022-07-02
Fuselage - Tail Boom Spar Caps - Inspection / Removal
The Federal Register Volume 87, Number 64, Final Rule titled "Fuselage - Tail Boom Spar Caps - Inspection / Removal" is an airworthiness directive issued by the FAA for certain Bell Textron Inc. helicopters including Models 205A, 205A-1, 205B, 210, 212, 412, 412CF, and 412EP equipped with tailboom left hand fin spar cap part number 212-030-447-117. This directive addresses the detection and removal of cracked spar caps to ensure continued airworthiness and safety.
Airworthiness DirectiveMaintenanceSafety MgmtBell Textron Inc. (Bti) 205Bell Textron Inc. (Bti) 210Bell Textron Inc. (Bti) 212Bell Textron Inc. (Bti) 412Bell Textron 205ABell Textron 205A-1Bell Textron 205BBell Textron 210Bell Textron 212Bell Textron 412Bell Textron 412CFBell Textron 412EP