COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes
AD/SA-TP/19 Heat Exchange Unit Intensifier Tube NK
Applicability: All series 1 and 3.
Document: Scottish Aviation TNS No. 26. Compliance: Forthwith.
Overview
The Civil Aviation Regulations 1998, as amended, are central to ensuring the safety and efficiency of civil aviation within Australia. One of the key legislative instruments under this act is the Airworthiness Directives (ADs) issued by the Civil Aviation Safety Authority (CASA). Specifically, AD/SA-TP/19 pertains to the British Aerospace (Scottish Aviation) Twin Pioneer Series aeroplanes, aiming to address potential safety concerns related to the heat exchange unit intensifier tube in series 1 and 3 aircraft. This directive was introduced to mitigate risks associated with the identified issue, ensuring that all affected aircraft meet stringent safety standards. The policy objective, as stated within the text, is to mandate compliance forthwith, ensuring that any identified safety risks are addressed without delay. This legislative instrument is enacted by the Commonwealth of Australia, overseen by the relevant legislature and CASA, ensuring adherence to national and international aviation safety standards.
Scope and Application
The Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives pertains to the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes and specifically addresses the heat exchange unit intensifier tube, as outlined in AD/SA-TP/19. This directive applies to all aircraft within the Twin Pioneer Series 1 and 3, necessitating immediate compliance as specified in Scottish Aviation Technical Notice No. 26. The regulation falls under the purview of the Commonwealth of Australia and is governed by the Civil Aviation Regulations 1998, with its jurisdictional reach extending across the national airspace. The directive applies to aircraft operators, maintenance personnel, and any entities involved in the operation or maintenance of the affected aircraft models. The scope of the directive ensures that all relevant stakeholders adhere to the stipulated requirements to maintain airworthiness standards, without any stated exclusions or exemptions in this particular directive. CASA may extend or further specify the application of this directive through subordinate instruments or additional notices.
Key Provisions
The Civil Aviation Regulations 1998 (Regulations) under Part 39, particularly section 105, pertain to the Airworthiness Directives issued by the Civil Aviation Safety Authority (CASA). In this case, AD/SA-TP/19 pertains to the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes and specifically addresses the heat exchange unit intensifier tube for all series 1 and 3 aircraft (Section 105). The directive mandates that compliance with the requirements outlined in Scottish Aviation Technical Notice No. 26 must be achieved forthwith, meaning immediately or as soon as possible.
The Regulations impose a clear obligation on aircraft owners, operators, and maintenance providers to ensure that the heat exchange unit intensifier tube of the specified Twin Pioneer Series Aeroplanes is in compliance with the standards and modifications detailed in Scottish Aviation Technical Notice No. 26. This directive aims to maintain the airworthiness of the aircraft by addressing a specific component that, if not properly maintained, could pose a safety risk.
Failure to comply with the provisions of AD/SA-TP/19 can result in significant consequences. Under the Civil Aviation Act 1988, non-compliance with Airworthiness Directives can lead to enforcement actions by CASA. These actions may include the issuance of a Notice of Proposed Civil Penalty, which can result in fines of up to $210,000 for individuals and up to $1,050,000 for corporations. In more severe cases, CASA may seek prosecution through the courts, leading to heavier penalties and potential criminal charges. Additionally, non-compliance can result in the grounding of the aircraft, preventing it from operating until the required modifications or checks are completed. This can have substantial operational and financial implications for the aircraft owner or operator.