EASA Regulations for Bell Textron Inc. (Bti) 204B

2 airworthiness directives and regulatory documents affecting Bell Textron Inc. (Bti) 204B.

EASA AD US-2024-17-02

Fuselage — Tailboom Attachment — Inspection / Replacement

Fuselage — Tailboom Attachment — Inspection / Replacement is a regulatory document addressing the inspection and replacement requirements for the tailboom attachment on certain aircraft fuselages. The document outlines procedures to ensure structural integrity and safety of the tailboom attachment area. It applies to aircraft models equipped with this specific fuselage-tailboom configuration.

Oct 31, 2024

Airworthiness DirectiveMaintenanceSafety MgmtBell Textron Inc. (Bti) 204BBell Textron Inc. (Bti) 205Bell Textron Inc. (Bti) 210

EASA AD US-2024-19-17

Rotors Flight Control - Tension Torsion (TT) Straps - Removal / Installation Prohibition

The document titled 'Rotors Flight Control - Tension Torsion (TT) Straps - Removal / Installation Prohibition' is a regulatory directive addressing the handling of tension torsion straps in rotor flight control systems. It applies to specific rotorcraft models equipped with these components, prohibiting their removal or installation to ensure flight safety and structural integrity.

Sep 30, 2024

Safety DirectiveMaintenanceSafety MgmtBell Textron Inc. (Bti) 204BBell Textron Inc. (Bti) 205Bell Textron Inc. (Bti) 210Bell Textron Inc. (Bti) 212