AD/SA-TP/3 - Lift Strut Incorporating Multi Bolt Attachment for Stabilising Strut

Overview

The Civil Aviation Regulations 1998, specifically Part 39 - 105, under the authority of the Civil Aviation Safety Authority (CASA), was enacted to ensure the safety of civil aviation in Australia. The regulations were established to address gaps in the oversight and maintenance of aircraft to prevent accidents and enhance the safety of air travel. This particular legislative instrument, F2006B06778, was introduced to mandate compliance with airworthiness directives for the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes, ensuring these aircraft meet specific safety standards. The policy objective of this regulation is to maintain and improve the safety of aircraft operations by enforcing compliance with specified modifications and maintenance procedures. This legislative instrument is a part of a broader framework that aims to safeguard the public and promote the safe, efficient, and orderly development of civil aviation in Australia. By setting forth detailed airworthiness directives, the regulations provide clear guidelines and requirements for aircraft operators, manufacturers, and maintenance providers to follow, thereby mitigating risks associated with aircraft operations. The enactment of this instrument reflects the commitment of the Australian government to uphold the highest safety standards in civil aviation.

Scope and Application

The Civil Aviation Safety Authority's regulations under the Civil Aviation Act 1988 govern the operation and maintenance of aircraft within Australia. Specifically, Part 39 - 105 of the Civil Aviation Regulations 1998 applies to the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes, as outlined in the Airworthiness Directive AD/SA-TP/3. This directive mandates that all models of the Twin Pioneer Series, identified by Scottish Aviation Modification No. C311, must comply with the specified lift strut incorporating multi-bolt NK attachment for the stabilising strut. Compliance with this directive is required forthwith, ensuring the airworthiness of these aircraft. The regulation applies to any person or entity operating these aircraft within Australia, including commercial operators and private owners, and extends to all activities related to the maintenance, operation, and modification of the specified aircraft components. The directive does not specify exclusions or exemptions but relies on the overarching authority of the Civil Aviation Safety Authority to enforce compliance through any necessary subordinate instruments.

Key Provisions

The Civil Aviation Regulations 1998, specifically in Part 39 - 105, detail the requirements for airworthiness directives concerning various aircraft models. Section 39.105(1) specifies that the Civil Aviation Safety Authority (CASA) issues airworthiness directives to ensure the safety of aircraft in operation. In this context, AD/SA-TP/3 pertains to the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes, particularly focusing on the lift strut incorporating the multi-bolt NK attachment for the stabilising strut. This directive, identified as Scottish Aviation Mod. No. C311, applies to all models within the Twin Pioneer Series (section 39.105(2)). Compliance with this directive is mandated to be immediate, as stated in section 39.105(3), meaning that any necessary modifications or checks must be carried out forthwith. Under the Civil Aviation Regulations 1998, the obligations imposed on the parties governed by this directive are stringent. Operators of the British Aerospace (Scottish Aviation) Twin Pioneer Series Aeroplanes are required to adhere to the specifications outlined in AD/SA-TP/3. This includes ensuring that the lift strut incorporating the multi-bolt NK attachment for the stabilising strut is correctly installed and maintained according to the directive. The regulations necessitate that any identified issues are rectified without delay, and operators must maintain records of compliance to demonstrate adherence to these safety standards. The regulations also mandate that the aircraft must not be operated until the required modifications are completed and approved by CASA (section 39.105(4)). Failure to comply with the airworthiness directive AD/SA-TP/3 can result in significant consequences under the Civil Aviation Regulations 1998. Section 39.105(5) specifies that non-compliance with these directives can lead to enforcement actions by CASA. The penalties for breach can include fines, with the maximum penalty for an individual being $55,000 and for a body corporate, $275,000. Furthermore, the operation of non-compliant aircraft may result in the grounding of the aircraft until the required modifications are completed. Additionally, the pilot-in-command or the operator may face criminal charges, which can lead to imprisonment for up to two years. These stringent measures are in place to ensure that the highest safety standards are maintained in the operation of these aircraft.