EASA Regulations for Bell Textron 205A

2 airworthiness directives and regulations affecting Bell Textron 205A.

EASA AD US-2024-16-01

Fuselage - Tail Boom Attachment Cap Angle - Inspection

The Federal Aviation Administration's Airworthiness Directive 2024-16-01 is a final rule addressing Bell Textron Inc. helicopters, including Models 412, 412CF, 412EP, 212, 205A, 205A-1, and 205B. It mandates inspections of the tail boom attachment cap angle and adjacent structures for cracks to prevent potential failure and loss of helicopter control. This directive updates previous requirements and incorporates new inspection procedures and reporting obligations.

Aug 22, 2024

Airworthiness DirectiveMaintenanceSafety MgmtBell Textron Inc. (Bti) 205Bell Textron Inc. (Bti) 212Bell Textron Inc. (Bti) 412Bell Textron 412Bell Textron 412CFBell Textron 412EPBell Textron 212Bell Textron 205ABell Textron 205A-1Bell Textron 205B

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.

Apr 6, 2022

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