Airworthiness Directives 2004 - Revocation and Remaking - Brantly B-2 Series Helicopters

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 Airworthiness Directives 2004

 I, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety

 Authority, acting under subregulation 39.001 (1) of the Civil

 Aviation Safety Regulations 1998:

 (a) revoke the Airworthiness Directives mentioned in

 Schedule 1; and

 (b) make, as separate instruments, each Airworthiness

 Directive mentioned in Schedule 1 and attached.

 

 

 David Villiers

 Delegate of the Civil Aviation Safety Authority

 

  20 December 2004

 Note:   Each attached Airworthiness Directive is being re-made in exactly the

 same form as appears in the latest published edition of the Directive.

 


 Schedule 1 Revocation and Remaking of

 Airworthiness Directives

 Brantly B-2 Series Helicopters

 AD Name AD Number

 Tail Rotor Guard and Skid Assembly P/N B2-416 - Modification AD/B-2/1

 Tail Rotor Drive - Modification AD/B-2/2

 Tail Rotor Drive - Inspection AD/B-2/3

 Tail Rotor Drive - Modification AD/B-2/4

 Tail Cone Reinforcement AD/B-2/5

 Overunning Clutch - Modification and Cockpit Placard Amendment AD/B-2/6

 Main Rotor Blade Dampers - Installation AD/B-2/7

 Tail Cone Reinforcement AD/B-2/8

 Main Transmission Mount - Reinforcement AD/B-2/9

 Rotor Blade Hinge - Modification AD/B-2/10

 Tail Rotor Blade Retaining Nut - Safetying AD/B-2/11

 Main Transmission Forward Mount - Rework AD/B-2/12

 Tail Rotor Guard - Inspection AD/B-2/13

 Rod End Bearings (Old Type KAHR. HE3SFN) on Forward End of U/C Drag  AD/B-2/14

 Superseded by AD/B-2/23 AD/B-2/15

 Centrifugal Clutch - Inspection Cockpit Placard - Installation AD/B-2/16

 Elimination of Carburettor Manifold From Oil System AD/B-2/17

 Seat Safety Bracket - Installation AD/B-2/18

 Transmission Mount Lugs - Reinforcement AD/B-2/19

 Increased Tail Rotor Control - Modification AD/B-2/20

 Conversion of Fuel Pump Model RD 7790D3 and E to G AD/B-2/21

 Seat Back Adjustment Wire - Removal AD/B-2/22

 Main Rotor Blades - Inspection and Replacement AD/B-2/23

 Rudder Control Post Upper Attachment - Modification AD/B-2/24

 Tail Rotor Blade - Inspection AD/B-2/25

 Main Rotor Mast Upper Bearing - Replacement AD/B-2/26

 Tail Rotor Blades Strike Indicators - Installation AD/B-2/27

 Tail Rotor Blade Spar - Inspection AD/B-2/28 Amdt 1

 Tail Rotor Drive Shaft - Inspection and Corrosion Proofing AD/B-2/29 Amdt 1


 Retirement Life - Critical Components AD/B-2/30 Amdt 3

 Main Rotor Mast - Inspection AD/B-2/31

 

Overview

The Airworthiness Directives 2004 is a legislative instrument enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, under the authority of subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The directive aims to revoke and remake various Airworthiness Directives concerning the Brantly B-2 Series Helicopters, ensuring they align with the latest safety standards and regulatory requirements. The policy objective behind these directives is to maintain and enhance the airworthiness of the specified aircraft, thereby safeguarding the safety of the public and aviation personnel. This legislative instrument was enacted to address the need for updated and consistent airworthiness directives in response to evolving safety concerns and technological advancements in the aviation industry. By remaking these directives, the Civil Aviation Safety Authority ensures that all relevant stakeholders are provided with the most current safety requirements and modifications necessary for the Brantly B-2 Series Helicopters. The directives are meticulously crafted to reflect the latest published editions, thereby maintaining a high standard of safety and compliance in the aviation sector.

Scope and Application

The Airworthiness Directives 2004, issued by the delegate of the Civil Aviation Safety Authority under the Civil Aviation Safety Regulations 1998, applies specifically to the Branly B-2 Series Helicopters. This legislative instrument revokes and remakes various Airworthiness Directives concerning specific modifications, inspections, and safety improvements for these helicopters. The geographic and jurisdictional reach of these directives is national, as they pertain to the civil aviation safety standards enforced by the Commonwealth of Australia. The directives outline specific technical requirements and safety measures that must be adhered to by the operators of Branly B-2 Series Helicopters, ensuring that these aircraft maintain airworthiness and comply with the prescribed safety standards. The application is limited to the specified modifications and inspections listed in the attached directives and does not extend to other aircraft models or types of aviation equipment.

Key Provisions

The Airworthiness Directives 2004 primarily focuses on the revocation and remaking of specific airworthiness directives related to the Brantly B-2 Series Helicopters (section 2). This legislative instrument revokes the previously mentioned airworthiness directives listed in Schedule 1 and subsequently re-makes them as separate instruments, maintaining their original form as per the latest published editions. These directives include a range of modifications, inspections, and safety amendments relevant to various components of the helicopter, such as the tail rotor guard, tail rotor drive, tail cone reinforcement, and main rotor blade dampers, among others. The Act imposes specific obligations and requirements on the entities governed by these airworthiness directives. Aircraft operators and maintenance organisations must ensure compliance with the newly remade directives, which involve implementing the specified modifications, conducting necessary inspections, and adhering to safety placard amendments. The directives are designed to enhance the airworthiness and safety standards of the Brantly B-2 Series Helicopters, thereby reducing the risk of accidents and ensuring the continued safe operation of these aircraft. Breach of the airworthiness directives may result in various civil and criminal consequences. Non-compliance with the mandated modifications and inspections could lead to the grounding of the aircraft, thereby affecting the operational capacity of the operator. Furthermore, serious breaches may attract regulatory action from the Civil Aviation Safety Authority, including fines and potential legal proceedings. The maximum penalties for such breaches are not explicitly stated in the legislative instrument but would be governed by the relevant aviation safety regulations and any applicable aviation-related legislation. Ensuring adherence to these directives is critical for maintaining the airworthiness and safety of the Brantly B-2 Series Helicopters within the Australian aviation sector.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.