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
Reims Aviation F406 Series Aeroplanes
AD Name AD Number
Canted Rib Upper Cap AD/F406/1
Aircraft Flight Manual, Flight into Icing Conditions AD/F406/2 Amdt 1
NLG Steering Cable and Air Conditioning Relay AD/F406/3
Engine Fuel Lines AD/F406/4
Horizontal Stabiliser Rear Attach Structure AD/F406/5
Elevator Forward Spar AD/F406/6
Nose Landing Gear Actuator Attach Structure AD/F406/7
Forward and Aft Facing Seat Identification AD/F406/8
Flap Control System Pushrod AD/F406/9
Fuel Boost Pump Wiring AD/F406/10
Fuselage to Center Wing Connection AD/F406/11
Overview
The Airworthiness Directives 2004 were enacted to ensure the continuing airworthiness of aircraft in Australia, specifically revoking and remaking certain Airworthiness Directives for Reims Aviation F406 Series Aeroplanes. This legislative instrument was made under the authority of David Alan Villiers, a delegate of the Civil Aviation Safety Authority, pursuant to subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The objective was to update and standardise the regulatory framework for airworthiness by replacing outdated directives with current versions, ensuring that all safety standards are uniformly applied and maintained. The revocation and remaking of these directives aimed to address any discrepancies or outdated specifications within the previous directives, thereby enhancing the safety and reliability of the aircraft in question.
Scope and Application
The Airworthiness Directives 2004, issued under the authority of David Alan Villiers, a delegate of the Civil Aviation Safety Authority, pertains to the revocation and re-making of various Airworthiness Directives applicable to specific aircraft models, particularly the Reims Aviation F406 series aeroplanes. This legislation applies to aircraft manufacturers, operators, maintenance personnel, and any other entities involved in the production, operation, or maintenance of the specified aircraft models. The geographic reach of this Act is national, as it concerns the safety standards within Australia's civil aviation sector. Each Airworthiness Directive is re-made in the same form as it appears in the latest published edition, ensuring the continued application of updated safety regulations. There are no stated exclusions or exemptions within the text, indicating that all specified aircraft must comply with the outlined directives. Subordinate instruments may further extend or restrict the application of these directives by detailing specific compliance requirements or enforcement measures.
Key Provisions
The primary sections of this legislative instrument, "Airworthiness Directives 2004", include the revocation and remaking of specific Airworthiness Directives related to Reims Aviation F406 Series Aeroplanes. Section 1 provides for the revocation of the previously existing Airworthiness Directives, which are listed in Schedule 1 (1). Section 2 then mandates the remaking of these directives in exactly the same form as they appear in the latest published edition, also detailed in Schedule 1 (2). This ensures that the most current and accurate safety requirements are applied to the specified aircraft.
The obligations and requirements imposed by this Act on the parties it governs are primarily centered around ensuring the airworthiness and safety of Reims Aviation F406 Series Aeroplanes. Owners, operators, and maintenance personnel must comply with the specific directives detailed in the remade Airworthiness Directives. These directives cover various aspects of the aircraft, such as the aircraft flight manual for flight into icing conditions, NLG steering cable, air conditioning relay, engine fuel lines, horizontal stabiliser rear attach structure, elevator forward spar, nose landing gear actuator attach structure, forward and aft facing seat identification, flap control system pushrod, fuel boost pump wiring, fuselage to center wing connection, and so forth. Each of these directives outlines specific actions and procedures that must be followed to maintain compliance with safety standards.
Failure to comply with the provisions of these Airworthiness Directives can result in significant consequences. While the specific offences and penalties are not detailed in the legislative instrument, non-compliance with airworthiness directives generally falls under civil aviation regulations, which may include fines, penalties, or other enforcement actions. Non-compliance could potentially lead to grounding of the aircraft, suspension or revocation of air operator certificates, or other regulatory actions deemed necessary to ensure safety. The exact penalties would be determined in accordance with the Civil Aviation Safety Regulations 1998 and other relevant legislation.