EASA Regulations for Bell Textron Inc. (Bti) 210

8 airworthiness directives and regulations affecting Bell Textron Inc. (Bti) 210.

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New ADs and bulletins for Bell Textron Inc. (Bti) 210, summarized like the ones below, every Monday.

EASA AD US-2024-20-07

Nov 29, 2024

Equipment / Furnishings - Emergency Float Kit Activation Handle - Repetitive Inspections / Replacement

The document titled 'Equipment / Furnishings - Emergency Float Kit Activation Handle - Repetitive Inspections / Replacement' is a regulatory directive addressing the maintenance requirements for the emergency float kit activation handle on certain aircraft. It mandates repetitive inspections and replacement procedures to ensure the proper functioning of this critical safety equipment. The directive applies to aircraft equipped with the specified emergency float kit activation handle assemblies.

Airworthiness Directive
  • Airbus Helicopters AS 350
  • Airbus Helicopters EC 130
  • Airbus Helicopters EC 120 B
  • Airbus Helicopters BO 105
  • Airbus Helicopters EC135
  • Airbus Helicopters 635
  • Airbus Helicopters MBB-BK 117
  • Bell 206
  • Bell 407
  • Bell Textron Inc. (Bti) 210
  • Bell Textron Inc. (Bti) 212
  • Bell Textron Inc. (Bti) 412
  • Leonardo S.P.A. Helicopters AB212
  • Leonardo S.P.A. Helicopters AB412
  • Md Helicopters Inc (Mdhi) 369
  • Md Helicopters Inc (Mdhi) 500N
  • Robinson R44 (Raven)
  • Robinson R66
  • Sikorsky S-76

EASA AD US-2024-17-02

Oct 31, 2024

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.

Airworthiness Directive
  • Bell Textron Inc. (Bti) 204B
  • Bell Textron Inc. (Bti) 205
  • Bell Textron Inc. (Bti) 210

EASA AD US-2024-19-17

Sep 30, 2024

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.

Safety Directive
  • Bell Textron Inc. (Bti) 204B
  • Bell Textron Inc. (Bti) 205
  • Bell Textron Inc. (Bti) 210
  • Bell Textron Inc. (Bti) 212

EASA AD US-2022-20-14

Nov 29, 2022

Main Rotor Drive - Main Transmission Housing Assembly - Inspection

Airworthiness Directive 2022-20-14 is a final rule issued by the Federal Aviation Administration addressing Bell Textron Inc. helicopters including models 204B, 205A, 205A-1, 205B, 210, 212, 412, 412CF, 412EP, and various restricted category helicopters. This directive mandates repetitive inspections of the main transmission housing assembly for cracks, corrosion, and pitting due to reported cracks in the main transmission support case. The directive aims to ensure continued airworthiness and safety of these helicopter models by identifying and correcting potential structural issues.

Airworthiness Directive
  • Bell Textron Inc. (Bti) 204B
  • Bell Textron Inc. (Bti) 205
  • Bell Textron Inc. (Bti) 210
  • Bell Textron Inc. (Bti) 212
  • Bell Textron Inc. (Bti) 412
  • Bell 204B
  • Bell 205A1
  • Bell 205B
  • Bell 210
  • Bell 212
  • Bell 412
  • Bell 412CF
  • Bell 412EP

EASA AD US-2022-22-12

Nov 10, 2022

NOT ADOPTED - EASA DECISION ATTACHED

The document titled NOT ADOPTED - EASA DECISION ATTACHED is an official position from EASA regarding FAA Airworthiness Directive 2022-22-12. This FAA AD applies to certain helicopters modified by FAA STC SR01298NY, including Bell Textron Inc. type designs and Leonardo AB412 helicopters. EASA has determined that FAA AD 2022-22-12 is not eligible for adoption within the European Union because the FAA STC SR01298NY is not validated by EASA for all affected helicopter types, specifically Leonardo AB412 helicopters.

Agency Decision
  • Bell Textron Inc. (Bti) 204B
  • Bell Textron Inc. (Bti) 205
  • Bell Textron Inc. (Bti) 210
  • Bell Textron Inc. (Bti) 212
  • Bell Textron Inc. (Bti) 412
  • Leonardo S.P.A. Helicopters AB212
  • Leonardo S.P.A. Helicopters AB412
  • Mcdermott 214 Holdings, 214
  • Bell Textron Inc. Helicopter
  • Leonardo AB412

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

EASA AD US-2022-06-03

Mar 15, 2022

Main Rotor - Hub Strap Pins - Removal / Inspection

The Federal Aviation Administration's Airworthiness Directive 2022-06-03 addresses safety concerns for Bell Textron Inc. helicopters, specifically Models 204B, 205A, 205A-1, 205B, 210, and 212 equipped with main rotor hub strap pins part number 204-012-104-005 with serial number prefix "FNFS". This directive mandates removal and inspection of all affected pins, both outboard and inboard, to prevent potential main rotor blade detachment. It also requires removing the mating strap fitting if any deformation is found on the pins.

Airworthiness Directive
  • Bell Textron Inc. (Bti) 204B
  • Bell Textron Inc. (Bti) 205
  • Bell Textron Inc. (Bti) 210
  • Bell Textron Inc. (Bti) 212
  • Bell 204B
  • Bell 205A1
  • Bell 205B
  • Bell 210
  • Bell 212

EASA AD US-2022-02-02

Feb 9, 2022

Superseded by FAA AD 2022-06-03

FAA Airworthiness Directive 2022-02-02 is a final rule addressing unsafe conditions in Bell Textron Inc. Model 204B, 205A, 205A-1, 205B, 210, and 212 helicopters. It targets defective main rotor hub strap pins, part number 204-012-104-005 with serial number prefix "FNFS", which have been linked to a fatal accident due to pin failure causing rotor detachment.

Airworthiness Directive
  • Bell Textron Inc. (Bti) 204B
  • Bell Textron Inc. (Bti) 205
  • Bell Textron Inc. (Bti) 210
  • Bell Textron Inc. (Bti) 212
  • Bell Textron Inc. 204B
  • Bell Textron Inc. 205A1
  • Bell Textron Inc. 205B
  • Bell Textron Inc. 210
  • Bell Textron Inc. 212