EASA Regulations for Bell Textron 205A

2 airworthiness directives and regulations affecting Bell Textron 205A.

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New ADs and bulletins for Bell Textron 205A, summarized like the ones below, every Monday.

EASA AD US-2024-16-01

Aug 22, 2024

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.

Airworthiness Directive
  • Bell Textron Inc. (Bti) 205
  • Bell Textron Inc. (Bti) 212
  • Bell Textron Inc. (Bti) 412
  • Bell Textron 412
  • Bell Textron 412CF
  • Bell Textron 412EP
  • Bell Textron 212
  • Bell Textron 205A1
  • Bell Textron 205B

EASA AD US-2022-07-02

Apr 6, 2022

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 Directive
  • Bell Textron Inc. (Bti) 205
  • Bell Textron Inc. (Bti) 210
  • Bell Textron Inc. (Bti) 212
  • Bell Textron Inc. (Bti) 412
  • Bell Textron 205A1
  • Bell Textron 205B
  • Bell Textron 210
  • Bell Textron 212
  • Bell Textron 412
  • Bell Textron 412CF
  • Bell Textron 412EP