Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, represent a comprehensive framework designed to ensure the safety and efficiency of civil aviation within the country. One aspect of this regulation is the 1998 Act's Schedule of Airworthiness Directives, which includes specific requirements and amendments for various aircraft models to ensure ongoing compliance with safety standards. The Civil Aviation Safety Authority (CASA) issues these directives to address particular safety concerns or to update existing standards in response to new information or technological advancements. The policy objective of these regulations is to maintain the highest possible safety standards in civil aviation, thereby protecting passengers, crew, and the general public from potential hazards associated with aircraft operations. One example of such an amendment is found in Part 39 - 105 of the Civil Aviation Regulations 1998, specifically relating to the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes. The amendment, AD/SA-TP/26 Amendment 1, focuses on the flap operating system of these aircraft. This amendment mandates compliance with the Scottish Aviation Technical Notice 50 issue 3, requiring action to be taken within 200 hours of time in service after the last compliance with the previous issue of this directive, dated before 31 January 1987, and thereafter every 200 hours of time in service. This update reflects the latest technical notice, extending the compliance period to ensure continued adherence to safety standards.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority Schedule of Airworthiness Directives, governing the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes. This regulation applies to all models of the specified aircraft series and mandates compliance with Scottish Aviation Technical Notice 50, Issue 3, concerning the flap operating system. The directive requires action to be taken within 200 hours of time in service after the last compliance with the previous issue of this directive before 31 January 1987, and subsequently every 200 hours of time in service. This amendment aims to incorporate the latest technical notice, thereby extending compliance requirements to 200 hours of time in service. The scope of this directive encompasses all entities operating the Twin Pioneer Series Aeroplanes within the Commonwealth of Australia, ensuring adherence to the specified airworthiness standards set forth by the Civil Aviation Safety Authority.

Key Provisions

The primary sections of this legislative instrument (AD/SA-TP/26 Amendment 1) pertain to the applicability of the Airworthiness Directives for the British Aerospace (Scottish Aviation) Twin Pioneer Series aeroplanes. Section 1 of the amendment specifies that it applies to all models of the Twin Pioneer aeroplanes. The directive focuses on the flap operating system, with Section 1/87 outlining the requirement for compliance with Scottish Aviation Technical Notice (TNS) 50, issue 3. The compliance requirement is detailed in Section 1/87, which mandates that action be taken in accordance with this technical notice within 200 hours of time in service after the last compliance with the previous issue of the directive prior to 31 January 1987, and subsequently every 200 hours of time in service. The obligations imposed by this Act on the parties and entities it governs are centred around ensuring the continued airworthiness of the Twin Pioneer aeroplanes. Operators and owners of these aircraft are required to adhere strictly to the compliance schedule as specified in the directive. Specifically, they must ensure that the flap operating system is inspected and maintained in accordance with the guidelines provided in Scottish Aviation TNS 50, issue 3. This includes conducting the necessary checks and maintenance within the specified timeframes to avoid any lapse in compliance. Failure to comply with the provisions of this directive can result in various consequences. While the specific civil or criminal penalties are not explicitly stated in this section of the legislation, non-compliance with airworthiness directives can generally lead to enforcement actions by the Civil Aviation Safety Authority (CASA). These actions can include fines, suspension of the aircraft's certificate of airworthiness, or even grounding of the aircraft until the required compliance is achieved. Such measures are intended to ensure that the safety standards set by the regulations are upheld, thereby protecting the safety of all persons on board and on the ground.