AD/AUS/2 - Tail Attachment Bolts

Overview

The Civil Aviation Regulations 1998, specifically under Part 39 - 105 of the Civil Aviation Safety Authority Schedule of Airworthiness Directives, address the safety standards and operational requirements for civil aviation in Australia. This legislative instrument, F2006B02571, was enacted to ensure that all aircraft, including the Auster/Beagle A.61 Series Aeroplanes, meet specific safety criteria. The problem it addresses includes ensuring the structural integrity of older aircraft models, particularly those manufactured before August 1947, through detailed maintenance and compliance protocols. The enacting body is the Parliament of the Commonwealth of Australia, with the policy objective of maintaining high safety standards in the civil aviation sector to protect the public and enhance operational reliability.

Scope and Application

The Civil Aviation Regulations 1998, as outlined in PART 39 - 105 and the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, apply specifically to Auster/Beagle A.61 Series Aeroplanes manufactured before August 1947. This legislation mandates that any person or entity responsible for the maintenance, operation, or ownership of these specific aircraft models must comply with the airworthiness directive AD/AUS/2 concerning the tail attachment bolts. The requirement necessitates adherence to the instructions provided in Auster SB Issue 7, with compliance expected forthwith. The directive's reach extends across the Commonwealth, ensuring a uniform standard of airworthiness and safety for these vintage aircraft within Australia. There are no stated exclusions or exemptions in this directive, meaning all applicable aircraft must meet the specified compliance criteria without exception. The regulations may be further refined or expanded upon through subordinate instruments issued by the Civil Aviation Safety Authority.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, address the airworthiness directives for Auster/Beagle A.61 Series Aeroplanes, with a focus on tail attachment bolts, as outlined in AD/AUS/2 (2/50). This directive applies to all Auster/Beagle A.61 Series aeroplanes manufactured before August 1947. The requirement is for the aeroplanes to be serviced in accordance with Auster Service Bulletin Issue 7, which details the necessary actions to ensure compliance. Compliance with these directives must be achieved forthwith, meaning immediately. The obligations imposed by this regulation on the owners, operators, and maintenance personnel of these aeroplanes are clear and specific. They must ensure that the maintenance and modification of the tail attachment bolts are carried out as per the instructions in Auster Service Bulletin Issue 7. This involves a thorough inspection, replacement, or repair of the bolts to meet the safety standards set forth by the Civil Aviation Safety Authority. Maintenance records must be updated to reflect the compliance with this directive, and the aeroplanes must be deemed airworthy by a certified aviation maintenance engineer. Failure to comply with the requirements of this airworthiness directive can result in serious consequences. The Civil Aviation Regulations 1998 stipulate that non-compliance may lead to the aeroplane being grounded until the necessary actions are taken. Furthermore, operators who fail to comply with the directive may face enforcement actions, including fines and potential criminal charges. The maximum penalties for breaches of these regulations can include significant financial penalties and, in severe cases, imprisonment. These measures are in place to ensure the highest standards of safety in the operation of civil aircraft within Australian airspace.