EASA AD US-2022-07-02
Apr 6, 2022Fuselage - 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