COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Radio Communication and Navigation Equipment
AD/RAD/8 Channel Tuning Mechanism AWA VHF Nav/Com
Receiver AD704 - Modification
Applicability: VHF NAV/COM Receiver type AD704. Manufacturers Reference C80071. Document: AWA Modification Procedure No. 10 Drawings 80071 D234-5.
Compliance: Before installation in an aircraft following next overhaul completed after 19 August 1963.
7/63
Overview
The Civil Aviation Regulations 1998, specifically Part 39, is a legislative instrument enacted by the Commonwealth of Australia to regulate and ensure the safety of civil aviation within Australian airspace. This legislation, overseen by the Civil Aviation Safety Authority, aims to establish and enforce standards for aircraft airworthiness and operational safety. One such standard is detailed in Airworthiness Directive AD/RAD/8, which pertains to the channel tuning mechanism of VHF NAV/COM Receiver type AD704, a critical component in aircraft radio communication and navigation systems. This directive was introduced to address the potential safety risks associated with the channel tuning mechanism of the specified receivers and aims to ensure that these systems comply with safety standards before installation following the next overhaul after 19 August 1963. The directive requires adherence to specific modification procedures, as outlined in AWA Modification Procedure No. 10, to maintain the integrity and reliability of the aircraft's navigation and communication capabilities.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 107, mandates the Airworthiness Directives concerning the radio communication and navigation equipment, particularly the AD/RAD/8 Channel Tuning Mechanism for AWA VHF Nav/Com Receiver AD704. This directive applies to the VHF NAV/COM Receiver type AD704, with the manufacturer's reference C80071, which must adhere to the modification procedure outlined in AWA Modification Procedure No. 10. The drawings for this modification are detailed in document 80071 D234-5. Compliance is required for any installation in an aircraft after the next overhaul completed following 19 August 1963, as specified in the directive dated 7/63. This legislation is applicable nationwide within the Commonwealth of Australia, extending its regulatory reach across all states and territories to ensure uniform safety standards in civil aviation. The directive is enforced by the Civil Aviation Safety Authority and can be extended or restricted through subordinate instruments as necessary, ensuring that the aviation industry maintains high standards of safety and reliability.
Key Provisions
The Civil Aviation Regulations 1998, particularly under Part 39 - 107, mandate that all modifications to radio communication and navigation equipment must adhere to the Airworthiness Directives (AD). Specifically, AD/RAD/8 addresses modifications to the channel tuning mechanism of the VHF NAV/COM Receiver type AD704. This AD applies to units manufactured with the reference C80071 and requires compliance with the AWA Modification Procedure No. 10. The compliance requirement is straightforward: any modifications must be completed before the next overhaul of the aircraft following 19 August 1963, as outlined in section 7/63.
The obligations imposed by this legislation are clear. Aircraft owners or operators must ensure that any modifications to the VHF NAV/COM Receiver AD704 are performed in accordance with the AWA Modification Procedure No. 10. This includes using the specified drawings (80071 D234-5) and ensuring that all modifications are completed before the next scheduled overhaul post-19 August 1963. Failure to comply with these directives could result in the aircraft being deemed non-airworthy, thereby rendering it ineligible for operation.
The consequences of non-compliance with these directives are significant. According to the Civil Aviation Regulations, failure to adhere to the Airworthiness Directives can result in civil penalties. Specifically, under section 87 of the Civil Aviation Act 1988, the maximum penalty for contravening these regulations can amount to $222,250 for individuals and $1,111,250 for corporations. Additionally, there could be criminal penalties, including imprisonment, if the non-compliance leads to a significant safety risk. Therefore, it is imperative for all stakeholders to strictly follow the AD/RAD/8 provisions to avoid any legal repercussions.