Airworthiness Directives 2004 - Revocation and Remaking - Pitts S-1 and S-2 Series Aeroplanes

Overview

The Airworthiness Directives 2004, made 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, was enacted to address the need for updating and maintaining compliance with airworthiness standards for specific aircraft models, particularly Pitts S-1 and S-2 series aeroplanes. The directive revoked previous airworthiness directives and remade them to ensure the latest safety standards and requirements are adhered to. The policy objective of this legislation is to ensure that all aircraft meet the necessary safety criteria, thereby enhancing the overall safety of civil aviation in Australia. This legislative instrument was made to provide clarity and consistency in the application of airworthiness directives, ensuring that operators of affected aircraft are fully aware of and comply with the updated safety requirements.

Scope and Application

The Airworthiness Directives 2004, made by David Alan Villiers as a delegate of the Civil Aviation Safety Authority under the Civil Aviation Safety Regulations 1998, primarily apply to the specific Pitts S-1 and S-2 series aeroplanes listed in the Schedule. These directives are intended to address particular safety concerns and modifications necessary to ensure the airworthiness of these aircraft. The legislation revokes previously issued directives and re-issues them as separate instruments, maintaining the original wording from the latest published editions. This legislative instrument operates within the Commonwealth jurisdiction, impacting aviation entities and individuals involved in the operation and maintenance of the specified Pitts aeroplanes across Australia. The directives outline specific requirements and modifications related to various components of the aircraft, such as the horizontal stabiliser, aileron inter-connect tube, and rudder control cables, among others. These directives are mandatory for compliance by the relevant entities, and non-compliance could result in legal repercussions under the Civil Aviation Safety Regulations 1998.

Key Provisions

The Airworthiness Directives 2004, made by David Alan Villiers, the delegate of the Civil Aviation Safety Authority (CASA), primarily involve the revocation and remaking of certain airworthiness directives (AD) that govern specific aircraft, in this case, the Pitts S-1 and S-2 Series Aeroplanes (section 1). The revocation of these directives (section 1(a)) is paired with their remaking as separate instruments (section 1(b)), ensuring that each directive is re-established in its most recent form as published. The detailed list of directives to be revoked and remade is set out in Schedule 1. These directives pertain to various modifications and inspections required for different components of the Pitts S-2 aircraft, such as the horizontal stabiliser, aileron inter-connect tube, rudder cables, and others. The obligations imposed by these airworthiness directives are significant for aircraft owners, operators, and maintenance personnel. They must ensure that all specified modifications and inspections are carried out as detailed in the re-made directives. This includes adhering to the exact specifications and procedures outlined for each component of the Pitts S-2 aeroplanes to maintain their airworthiness. Failure to comply with these requirements can lead to serious safety issues and non-compliance with aviation safety regulations. It is essential that all parties involved understand and implement the directives meticulously to ensure the continued safe operation of the aircraft. Breaching the provisions of these airworthiness directives can result in both civil and criminal consequences. Under Australian aviation law, non-compliance with airworthiness directives can be considered a breach of regulations, potentially leading to enforcement actions by CASA. Civil penalties may include fines, and in severe cases, aircraft may be grounded until compliance is achieved. Moreover, individuals responsible for ensuring compliance, such as aircraft owners or maintenance personnel, may face prosecution under the Civil Aviation Act 1988, which can result in substantial fines and even imprisonment. The exact penalties depend on the severity of the breach and the specific circumstances, but the potential for significant legal repercussions underscores the importance of strict adherence to these directives.