Airworthiness Directives 2004 - Revocation and Remaking - Eurocopter BK 117 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

 Eurocopter BK 117 Series Helicopters

 AD Name AD Number

 Tail Rotor Blade Bonding AD/GBK 117/1 Amdt 1

 Retirement Life - Critical Components - CANCELLED AD/GBK 117/2 Amdt 2

 Cowling Latches AD/GBK 117/3 Amdt 1

 Landing Gear Electrical Bonding AD/GBK 117/4

 Electrical Bonding and Static Dischargers AD/GBK 117/5

 Main Rotor Blade AD/GBK 117/6 Amdt 2

 Retrofit of Engine Overspeed Controller AD/GBK 117/7

 Tail Boom Vertical Fin Spar AD/GBK 117/8 Amdt 2

 Rotor Mast Assembly AD/GBK 117/9

 Introduction of a Life Limit on Tail Rotor Drive Bevel Gear AD/GBK 117/10

 Tension-Torsion Straps AD/GBK 117/11 Amdt 1

 Transmission and Engine Cowling Hook System AD/GBK 117/12

 Vertical Fin Skin Panelling AD/GBK 117/13

 Tail Rotor Drive Bearings AD/GBK 117/14

 

Overview

The Airworthiness Directives 2004 are a legislative instrument that was enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. This instrument aimed to address specific issues related to the airworthiness of certain aircraft by revoking existing airworthiness directives and remaking them as separate instruments to ensure they remain current and relevant. The problem this legislation sought to address was the need for updated and precise regulatory measures to maintain the safety standards of air travel, specifically for Eurocopter BK 117 Series Helicopters. The policy objective, as implied by the instrument, is to ensure that the airworthiness directives are accurately and effectively enforced to mitigate any safety risks associated with the specified aircraft.

Scope and Application

The Airworthiness Directives 2004, issued under the authority of David Alan Villiers, delegate of the Civil Aviation Safety Authority, and pursuant to subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, serve to revoke and remake a series of airworthiness directives concerning Eurocopter BK 117 Series Helicopters. This legislative instrument applies specifically to the entities involved in the operation, maintenance, and modification of these helicopters, as well as any individuals or corporations responsible for ensuring their airworthiness. The geographic and jurisdictional reach of these directives is comprehensive, extending to all operations within Australia, thereby affecting all helicopter operators, maintenance providers, and aviation professionals operating under the Australian Civil Aviation Safety Regulations. The instrument includes detailed specifications and requirements for the maintenance, inspection, and alteration of specific components of the helicopters to ensure compliance with safety standards. These directives are made under the authority of the Civil Aviation Safety Authority, ensuring that all activities are governed by stringent safety protocols and regulatory oversight.

Key Provisions

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Authority (CASA), primarily serve to revoke and re-make existing airworthiness directives concerning the Eurocopter BK 117 Series Helicopters (sections 1 and 2). These directives address specific maintenance and operational requirements to ensure the safety of these aircraft. Each directive in Schedule 1 is revoked and then re-made in its current form, maintaining the integrity and applicability of the safety standards as published in the latest edition. The obligations imposed by these directives are stringent, requiring operators of the Eurocopter BK 117 Series Helicopters to adhere to detailed maintenance and operational protocols. These include the bonding of tail rotor blades (AD/GBK 117/1 Amdt 1), the retirement of critical components with defined life limits (AD/GBK 117/2 Amdt 2), and the retrofitting of engine overspeed controllers (AD/GBK 117/7). Each directive mandates specific actions such as inspections, repairs, and replacements to ensure the continued airworthiness of the aircraft. Breaching any of the provisions outlined in these directives can result in severe consequences. Civil penalties may be imposed for non-compliance, which can include fines and other regulatory actions. Furthermore, failure to adhere to these airworthiness directives could lead to the grounding of the aircraft, thereby impacting the safety and operational viability of the fleet. The exact penalties for each offence are detailed within the individual airworthiness directives, which may include substantial fines and potential criminal charges for more serious breaches. Each directive specifies the maximum penalties applicable for non-compliance. For instance, failure to follow the maintenance requirements for the tail rotor blade bonding could result in fines up to a certain amount as stipulated in the relevant sections. Additionally, operators found in breach of these directives might face legal actions that could lead to imprisonment for more severe violations. These penalties underscore the importance of strict adherence to the directives to maintain the highest standards of aviation safety.

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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.