Airworthiness Directives 2004 - Revocation and Remaking - Aerospatiale (Socata) TB9 and TB10 (Tobago) Series Aeroplanes

Overview

The Airworthiness Directives 2004 was enacted by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, under the authority granted by subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. This legislative instrument was introduced to ensure that airworthiness directives, which are critical for maintaining the safety standards of aircraft, are kept up-to-date and reflect the latest safety requirements. The primary objective of these directives is to address specific safety issues identified in certain aircraft models, thereby enhancing overall aviation safety. By revoking and remaking existing directives, this legislation aims to ensure that all safety-related modifications and inspections are accurately and comprehensively communicated to aviation stakeholders. The Airworthiness Directives 2004 specifically targets Aerospatiale (Socata) TB9 and TB10 (Tobago) Series Aeroplanes, detailing a range of airworthiness limitations and required modifications. The directives cover various aspects of the aircraft, including horizontal stabilizer rivets, stabilator inspections, wing flap deflections, and fuel system requirements, among others. Each directive is re-made to exactly match the latest published edition, ensuring clarity and precision in safety communication. This legislative action by the Civil Aviation Safety Authority underscores the commitment to maintaining high safety standards within the aviation sector.

Scope and Application

The Airworthiness Directives 2004, made under the authority of the Civil Aviation Safety Regulations 1998, apply to specific types of aircraft, namely the Aerospatiale (Socata) TB9 and TB10 (Tobago) Series Aeroplanes. These directives mandate specific airworthiness limitations, including inspections, modifications, and replacements of various components such as horizontal stabilizer rivets, engine mounts, fuel tanks, and safety belts, among others. These directives aim to ensure the safety and airworthiness of the specified aircraft types by addressing identified safety issues through detailed technical requirements. The application of these directives extends across the Commonwealth of Australia, as they are issued by the Civil Aviation Safety Authority (CASA), which has regulatory jurisdiction over civil aviation safety nationwide. The directives are comprehensive, covering numerous aspects of the aircraft's structure and systems, and they are designed to be applied uniformly to all affected aircraft within the specified series. There are no explicit exclusions or exemptions stated within the text, implying that all relevant aircraft must comply with the outlined directives. The directives are remade in exactly the same form as they appear in the latest published edition, ensuring consistency and clarity in their application.

Key Provisions

The legislative instrument F2006B07698, made under the authority of David Alan Villiers as the delegate of the Civil Aviation Safety Authority, primarily serves to revoke and re-make various Airworthiness Directives (ADs) pertaining to the Aerospatiale (Socata) TB9 and TB10 (Tobago) Series Aeroplanes. Specifically, section (a) of the instrument revokes the ADs listed in Schedule 1, while section (b) simultaneously re-makes these ADs as separate instruments, ensuring they are in the exact form as the latest published editions. These ADs encompass a comprehensive range of airworthiness limitations and requirements, each assigned a distinct AD number for identification and compliance purposes. The Act imposes a variety of obligations and requirements on the parties and entities it governs. These include mandatory inspections and modifications to various components of the aircraft, such as the horizontal stabilizer rivets, stabilator, wing flap deflection, and fuel tanks, among others. For instance, AD/TB10/1 requires the inspection and modification of horizontal stabilizer rivets, while AD/TB10/2 mandates the inspection and replacement of the stabilator and rear fuselage modification. These directives aim to ensure that the aircraft maintain a high standard of airworthiness and safety, thus safeguarding the interests of all stakeholders involved in aviation activities. Failure to comply with the provisions outlined in these ADs can lead to significant consequences. The legislative instrument does not explicitly detail the penalties or consequences for non-compliance within its text; however, under the broader Civil Aviation Safety Regulations 1998, breaches of airworthiness directives can result in severe civil and criminal penalties. Civil penalties may include fines, while criminal penalties could involve imprisonment, depending on the severity and impact of the non-compliance. These potential penalties underscore the importance of adhering strictly to the ADs to avoid legal repercussions and ensure the continued safe operation of the aircraft.