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
Robinson R44 Series Helicopters
AD Name AD Number
Cooling Fan AD/R44/1
Cyclic Control System AD/R44/2
Push-Pull Guide Tubes AD/R44/3
Placard to Prohibit Pushovers AD/R44/4
Low RPM Warning Unit AD/R44/5 Amdt 1
Main Rotor Gearbox AD/R44/6
Clutch Assembly AD/R44/7
Lateral Cyclic Trim Spring Shaft AD/R44/8
Oil Line Elbows AD/R44/9
Main Rotor Blade AD/R44/10 Amdt 1
Cyclic Control Pilots Grip Assembly AD/R44/11 Amdt 1
Auxiliary Fuel Tank Sump Drain - Shut Off Clamp AD/R44/12
Rotor Drive Yoke AD/R44/13
Wire Harness and Fuel Line Chafing AD/R44/14
Sprag Clutch AD/R44/15
Vertical-to-Horizontal Stabiliser Attach Channel AD/R44/16
Tail Rotor Pitch Control Assembly AD/R44/17
Main Rotor Blades AD/R44/18
Main Rotor Clutch Drive Shafts AD/R44/19
Main Rotor Swashplate and Tail Rotor Bolts AD/R44/20
Overview
The Airworthiness Directives 2004, enacted on 20 December 2004, were introduced by David Alan Villiers, acting as a delegate of the Civil Aviation Safety Authority (CASA) under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. This legislative instrument sought to address the need for ensuring the ongoing airworthiness of Robinson R44 Series helicopters by revoking and remaking existing Airworthiness Directives. The revocation and remaking of these directives were intended to bring them into alignment with the latest safety standards and practices, thus ensuring that the helicopters continue to meet the necessary safety requirements. The policy objective behind these directives is to enhance aviation safety by providing specific safety measures and compliance requirements for the operation of Robinson R44 Series helicopters.
Scope and Application
The Airworthiness Directives 2004, as re-made by David Alan Villiers, delegate of the Civil Aviation Safety Authority, targets specific maintenance and operational requirements for the Robinson R44 Series Helicopters. These directives apply to all helicopter operators and owners who hold or seek to hold an Australian Certificate of Airworthiness for the specified Robinson R44 models. The geographical scope of this legislation is nationwide, applying across the Commonwealth of Australia, ensuring consistent standards and practices in helicopter airworthiness and safety. The directives establish detailed technical specifications and mandatory actions regarding various components of the helicopters, including the cooling fan, cyclic control system, and main rotor gearbox, among others. Each directive is tailored to address identified safety concerns and is legally binding for those who operate the affected helicopters. Notably, these directives do not exclude any operator or helicopter within their scope, as they are integral to maintaining the airworthiness of the specified Robinson R44 models across the country.
Key Provisions
The Airworthiness Directives 2004 (F2006B08003) revokes existing directives pertaining to the Robinson R44 Series Helicopters and re-issues them as separate instruments. This legislative instrument outlines specific airworthiness requirements for various components of the helicopters, as detailed in the attached directives. These directives cover a range of systems and parts, including the cooling fan, cyclic control system, push-pull guide tubes, placards, low RPM warning unit, main rotor gearbox, clutch assembly, lateral cyclic trim spring shaft, oil line elbows, main rotor blade, cyclic control pilots grip assembly, auxiliary fuel tank sump drain, rotor drive yoke, wire harness and fuel line chafing, sprag clutch, vertical-to-horizontal stabiliser attach channel, tail rotor pitch control assembly, main rotor blades, main rotor clutch drive shafts, and main rotor swashplate and tail rotor bolts.
The obligations and requirements imposed by the Airworthiness Directives 2004 are primarily directed towards ensuring the safety and airworthiness of the Robinson R44 Series Helicopters. The directives detail specific maintenance, inspection, and repair protocols that must be followed for each component listed. For example, AD/R44/1 pertains to the cooling fan, requiring regular inspections and maintenance to prevent overheating. AD/R44/2 involves the cyclic control system, mandating periodic checks to ensure proper functionality. Each directive specifies the actions that must be taken, the frequency of inspections, and any required modifications or replacements. Failure to comply with these directives can result in the aircraft being deemed unairworthy.
Violations of the requirements set out in the Airworthiness Directives 2004 can lead to significant consequences. While the specific legal text does not detail the penalties, it is understood that non-compliance with airworthiness directives can result in substantial fines, enforcement actions, and potential criminal charges. Civil penalties for breaches of aviation safety regulations can include fines up to several thousand dollars, while criminal penalties can include imprisonment. The severity of the penalty often depends on the nature and extent of the breach, as well as any resulting harm or risk to safety.