Overview

The Civil Aviation Regulations 1998, amended through Legislative Instrument F2006B06345, are integral to the enforcement of aviation safety standards in Australia. These regulations, enacted by the Australian Parliament, were introduced to address the need for stringent safety protocols in the operation and maintenance of aircraft. Specifically, Part 39 – 105 of the Civil Aviation Regulations 1998 outlines the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, which includes AD/PROCTOR/6 concerning Percival Proctor Series Aeroplanes. This directive mandates the inspection of glued joints in the outer wings of all Mk. IV and Mk. V Proctors, ensuring that these components meet specified safety standards as per Percival Civil Technical Instruction No. 2. The policy objective is to maintain the airworthiness of these aircraft, thereby enhancing safety and reliability within the aviation sector.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority Schedule of Airworthiness Directives, applies to all Percival Proctor Series Aeroplanes, specifically the Mk. IV and Mk. V variants. The regulation mandates that the glued joints of all spar laminations in the outer wings must be inspected in accordance with Percival Civil Technical Instruction No. 2. This requirement is integral to ensuring the airworthiness and safety of these aircraft. Should the inspection uncover unsatisfactory results, the responsible party must notify the Department, which will then provide further instructions. The directive necessitates immediate compliance, underscoring the importance of timely and thorough inspections to maintain the safety standards set forth by the Civil Aviation Safety Authority. The scope of the legislation is explicitly territorial, applying to aircraft registered within the Commonwealth of Australia and operating under the oversight of the Civil Aviation Safety Authority. There are no stated exclusions or exemptions in this directive, and it extends its reach through the subordinate instrument, Percival Civil Technical Instruction No. 2.

Key Provisions

The Civil Aviation Safety Authority’s Schedule of Airworthiness Directives, specifically AD/PROCTOR/6(Re-Issue) (Section 6/50), mandates the inspection of the glued joints of all spar laminations in the outer wings of Percival Proctor Series Aeroplanes, both Mk. IV and Mk. V. This inspection must be conducted in accordance with Percival Civil Technical Instruction No. 2. If the results of the inspection are unsatisfactory, the Department must be notified of the details, and further instructions will be provided, as stipulated in DCA/PROCTOR/6 or A.N.O. 105.1.26.2.6.1. The directive requires that these inspections be carried out immediately. In terms of obligations, the directive imposes a clear and immediate requirement for operators and owners of Percival Proctor Series Aeroplanes to inspect the specified parts of their aircraft. The inspections must be thorough and adhere to the specified technical instructions. This directive does not leave much room for interpretation or delay; compliance is mandatory and must be achieved without undue delay. The onus is on the operators and owners to ensure that the inspections are carried out correctly and that any deficiencies identified are reported to the appropriate authorities without delay. Failure to comply with the provisions of AD/PROCTOR/6(Re-Issue) can lead to significant consequences. While the regulations do not explicitly state the penalties for non-compliance, it is reasonable to infer that non-compliance could result in severe repercussions under civil aviation law. These may include the grounding of the aircraft until the required inspections are completed and deficiencies are rectified, potential fines, and other enforcement actions by the Civil Aviation Safety Authority. Additionally, failure to adhere to airworthiness directives can have serious safety implications, potentially resulting in criminal charges if non-compliance leads to an accident or endangers flight safety. The exact penalties would be determined based on the severity of the breach and the impact on aviation safety.