AD/SA-TP/4 - Stabiliser Strut SA.B3.20.334

Overview

The Civil Aviation (Airworthiness) Regulations 1998, enacted in 1998, provide comprehensive guidelines for ensuring the airworthiness of aircraft in Australian airspace. This legislative instrument, amended by F2006B06779, addresses the need to maintain and enhance safety standards for civil aviation. The Australian Parliament established these regulations to ensure that all aircraft, including specific models such as the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes, comply with stringent safety and maintenance requirements. The policy objective is to safeguard public safety and preserve the integrity of civil aviation operations by enforcing stringent airworthiness directives and standards. Part 39 of the Civil Aviation Regulations 1998, specifically addressing the Stabiliser Strut SA.B3.20.334 for the Twin Pioneer Series Aeroplanes, aims to mandate immediate compliance with safety directives. The directive applies to all models within the specified series, identified by Scottish Aviation Mod. No. C319, and requires compliance forthwith. This regulation is integral to maintaining the safety and reliability of aircraft operations, ensuring that any potential structural issues are promptly addressed to prevent accidents and maintain the highest safety standards in civil aviation.

Scope and Application

The Civil Aviation Regulations 1998, as amended, under the jurisdiction of the Civil Aviation Safety Authority, apply comprehensively to all aspects of civil aviation within Australia. Specifically, PART 39 - 105, which pertains to the Schedule of Airworthiness Directives, mandates compliance with safety regulations for various aircraft models, including those in the British Aerospace (Scottish Aviation) Twin Pioneer Series. This particular directive, AD/SA-TP/4, targets the stabiliser strut SA.B3.20.334, as identified by the NK designation, and applies to all models of the Scottish Aviation Mod. No. C319. Compliance with this directive is required forthwith, ensuring that all relevant operators and maintenance personnel adhere to the stipulated safety standards to maintain the airworthiness of these aircraft. The geographic reach of this regulation is national, extending to all Commonwealth, state, and territory jurisdictions within Australia. Any exclusions, exemptions, or thresholds are detailed within the subordinate instruments linked to the primary regulation.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, contains crucial provisions for the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes, detailed under AD/SA-TP/4. This regulation mandates compliance with stabiliser strut SA.B3.20.334 NK for all models, with reference to the Scottish Aviation Modification No. C319 (section 1). Compliance is required forthwith, meaning that operators must adhere to these directives immediately without delay. Under this legislation, operators of the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes are required to ensure that the stabiliser strut SA.B3.20.334 NK is installed and maintained according to the specifications outlined in the Scottish Aviation Modification No. C319. This involves ensuring that all relevant documentation and modifications are completed and that the aeroplanes are airworthy as per the set standards (section 2). The regulation is clear that any deviation from these requirements can lead to serious safety implications. Failure to comply with the directives stipulated in AD/SA-TP/4 can result in significant consequences. The Civil Aviation Regulations 1998 outline that non-compliance may lead to enforcement actions, including the suspension or revocation of airworthiness certificates. Furthermore, operators found in breach of these provisions may face civil penalties, which can include substantial fines (section 3). In severe cases, criminal charges could also be pursued, leading to imprisonment for the responsible individuals or entities. The penalties for non-compliance with AD/SA-TP/4 are designed to ensure that operators take the required actions to maintain the airworthiness of their aircraft. The maximum civil penalty for contravening these regulations is substantial, reflecting the serious nature of the safety requirements. In addition to fines, criminal penalties can be imposed, with individuals potentially facing imprisonment, highlighting the importance of strict adherence to the legislated standards (section 4). The regulatory framework thus serves to protect public safety by ensuring that all Twin Pioneer Series Aeroplanes meet the necessary safety criteria.