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
Gulfstream (Rockwell) 112 Series Aeroplanes
AD Name AD Number
Aileron Hinge Doublers - Inspection and Modification AD/AC-112/1
Wing Structural Life Limitation AD/AC-112/2
Aileron Control System - Modification AD/AC-112/3
Engine Oil Pressure Line - Replacement AD/AC-112/4
Fuel Selector Valve - Inspection and Replacement AD/AC-112/5 Amdt 1
Front Seat and Shoulder Harness AD/AC-112/6 Amdt 4
Lower Vertical Fin Rib - Inspection AD/AC-112/7 Amdt 2
Aileron Hinge Supports - Inspection and Modification AD/AC-112/8 Amdt 1
Wing Structure - Rib - Inspection AD/AC-112/9
Fuel Tank Access Door Sealant - Replacement AD/AC-112/10
Elevator and Rudder Hinge Fittings - Inspection and/or Replacement AD/AC-112/11
Rudder Rib - Inspection AD/AC-112/12
Wing Forward Spar AD/AC-112/13 Amdt 2
Vertical Stabiliser Forward Spar Attachment Structure AD/AC-112/14 Amdt 1
Rudder Spar AD/AC-112/15
Overview
The Airworthiness Directives 2004 were enacted under the authority of David Alan Villiers, who is a delegate of the Civil Aviation Safety Authority, acting pursuant to subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The primary objective of these directives was to address existing issues and fill gaps in the airworthiness regulations concerning specific aircraft models, particularly the Gulfstream (Rockwell) 112 Series Aeroplanes. These directives were issued by the Australian Government's Civil Aviation Safety Authority to ensure that the relevant aircraft meet the necessary safety standards and compliance requirements. By revoking and remaking the existing airworthiness directives, the legislation aimed to update and enhance the regulatory framework governing aircraft safety in Australia, thereby ensuring that all aircraft operate under the most current and stringent safety standards.
Scope and Application
The Airworthiness Directives 2004 apply to the entities and persons involved in the operation, maintenance, and modification of Gulfstream (Rockwell) 112 Series Aeroplanes. This legislation governs the airworthiness standards that must be adhered to in ensuring the safety of these aircraft. The scope of the Act extends to the inspection, modification, and replacement of various aircraft components, including aileron hinges, wing structures, engine oil pressure lines, fuel selector valves, and more. The directives are made under the authority of the Civil Aviation Safety Authority and are in line with the Civil Aviation Safety Regulations 1998, ensuring compliance with national safety standards. The Act does not specify any exclusions or exemptions and is effective within the Commonwealth of Australia. Each directive is re-made in its entirety as it appears in the latest published edition, ensuring consistency and up-to-date safety requirements. The application of these directives is broad, covering all relevant aircraft and their operators within Australia.
Key Provisions
The Airworthiness Directives 2004 (F2006B07895) primarily focus on the revocation and remaking of various airworthiness directives concerning the Gulfstream (Rockwell) 112 series aeroplanes. These directives, listed in Schedule 1, pertain to specific maintenance and modification requirements for different parts of the aircraft, such as the ailerons, wing structures, engine oil pressure lines, and fuel systems, among others. The legislative instrument, signed by David Villiers, a delegate of the Civil Aviation Safety Authority (CASA), revokes the existing directives and simultaneously re-makes them as separate instruments to ensure continued compliance with the latest standards (sections 1(a) and 1(b)).
The obligations imposed by these directives on the parties governed, such as aircraft operators and maintenance providers, are significant. They are required to adhere to the specific inspection, modification, or replacement instructions outlined in each directive to ensure the continued airworthiness of the aircraft. This includes conducting regular inspections, making necessary repairs or modifications, and maintaining detailed records of compliance. These obligations are essential to ensure the safety and reliability of the aircraft in operation, thereby protecting both the passengers and crew on board (sections 1(a) and 1(b)).
Failure to comply with the provisions of these airworthiness directives can lead to serious legal consequences. Any breach of the requirements could result in civil or criminal penalties. For instance, operators who fail to comply with the mandated inspections and modifications could face substantial fines or even criminal charges, depending on the severity of the breach. The specific penalties are not detailed in the legislative instrument, but they are typically aligned with the Civil Aviation Safety Regulations 1998, which can impose significant financial penalties and, in severe cases, imprisonment for non-compliance. The overarching aim is to ensure that all parties governed by these directives maintain the highest safety standards in their operations (sections 1(a) and 1(b)).