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
Casa 212 Series Aeroplanes
AD Name AD Number
Fatigue Inspections and Retirement Lives AD/CASA/1 Amdt 5
Engine Firewall Sealing AD/CASA/2
Wing Flap Control Hinge Bearing - Replacement AD/CASA/3
Rudder Hinge Fittings - Modification AD/CASA/4 Amdt 1
Fuel Ejector Filter - Replacement AD/CASA/5
Fuel Shut-Off Valves - Replacement AD/CASA/6
Rudder Control System - Modification AD/CASA/7
Flight Controls - Fail-Safe Requirements AD/CASA/8
Engine Controls - Propeller Feathering System AD/CASA/9
Placard - Use of Reverse Thrust AD/CASA/10
Power Quadrant Cover AD/CASA/11
Flap Control Rod Joints AD/CASA/12
Flap Control System AD/CASA/13 Amdt 1
Propeller Speed and Pitch Control AD/CASA/14
Flight Idle Stops AD/CASA/15
Rudder Control AD/CASA/16
MLG Shock Absorber AD/CASA/17
Power Quadrant Slots AD/CASA/18
False Spar, Flap Housing Area AD/CASA/19
Corrosion of Rudder Torsion Tube AD/CASA/20
Corrosion Prevention and Control Programme (CPCP) AD/CASA/21
Inner Flap Fittings AD/CASA/22
Aileron Control Rod Movable Joint AD/CASA/23
Fuel Pump AD/CASA/24
SPZ4500 Autopilot Actuators AD/CASA/25
Overview
The Airworthiness Directives 2004, enacted by David Alan Villiers, delegate of the Civil Aviation Safety Authority, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, address the need to revoke and remake several existing Airworthiness Directives to ensure they remain current and effective. This legislative instrument aims to maintain the safety standards and regulatory compliance within Australia's aviation sector by updating and reissuing the directives in their latest form. The enactment is driven by the objective of ensuring that the airworthiness directives reflect the most recent safety requirements and technological advancements, thereby contributing to the overarching goal of enhancing aviation safety.
Scope and Application
The Airworthiness Directives 2004, made under the authority of the Civil Aviation Safety Regulations 1998, apply to specific CASA 212 Series Aeroplanes, detailing various maintenance and operational requirements. The directives focus on ensuring the continued airworthiness of these aircraft by addressing specific safety concerns, including fatigue inspections, engine firewall sealing, and various structural and control system modifications. These directives are binding on the operators and owners of the CASA 212 Series Aeroplanes, ensuring compliance with the detailed safety measures to maintain airworthiness standards. The geographic reach of these directives is national, applying across Australia, and they are enforced by the Civil Aviation Safety Authority. The legislation does not explicitly mention exclusions or exemptions but implies that non-compliance could lead to enforcement actions by the regulatory body. Subordinate instruments may extend or further detail the application of these directives, ensuring comprehensive coverage of safety requirements.
Key Provisions
The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Authority (CASA) and specifically referencing subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, primarily serves to revoke certain existing airworthiness directives and re-make them as separate instruments. This action is detailed in the Schedule 1 of the legislation, which lists the specific airworthiness directives being revoked and re-made. These directives pertain to various aspects of aircraft maintenance and operational safety, including fatigue inspections, engine firewall sealing, wing flap control, and more. The re-making of these directives ensures that they are presented in the same form as the latest published editions, thus maintaining consistency and clarity in safety standards.
The obligations imposed by these directives are significant and detailed, focusing on ensuring the safety and airworthiness of CASA 212 series aeroplanes. Each directive outlines specific maintenance actions, inspections, and modifications that must be carried out by aircraft operators and maintenance personnel. For example, AD/CASA/1 requires fatigue inspections and retirement lives for certain components, while AD/CASA/2 mandates the sealing of the engine firewall. Compliance with these directives is mandatory, and failure to adhere to the specified requirements could lead to severe safety risks. Operators must keep detailed records of compliance and ensure that all mandated inspections and modifications are completed within the prescribed timeframes.
Failure to comply with the provisions of these airworthiness directives can result in significant legal and financial consequences. The Civil Aviation Safety Regulations 1998 outline various penalties for non-compliance, which can include substantial fines and potential criminal charges. In cases where non-compliance leads to accidents or incidents, the consequences can be even more severe, including imprisonment for individuals found guilty of violating these safety standards. The maximum penalties for breaches of these directives can vary, but they are designed to enforce strict adherence to safety regulations and ensure that aircraft remain airworthy at all times. This stringent enforcement mechanism underscores the importance of these directives in maintaining the highest safety standards within the aviation industry.