AD/BEECH 23/2 - Rudder Leading Edge

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, form a comprehensive framework to regulate civil aviation safety, amongst other areas. One specific legislative instrument within this framework is the Airworthiness Directive AD/BEECH 23/2, issued under the authority of the Civil Aviation Safety Authority, which addresses safety concerns specific to Beechcraft 19, 23, and 24 series aeroplanes. This directive was introduced to rectify an identified safety issue concerning the rudder leading edge of these aircraft models. The policy objective of the directive is to ensure compliance with specific modifications as outlined in Hawker De Havilland Technical News Sheet Beech Aust. No. 2 Issue 1, specifically drawing 05/F/101, in order to maintain the airworthiness and safety standards of the affected aircraft.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 105, applies to all operators and owners of Beechcraft 19, 23 and 24 Series Aeroplanes, mandating adherence to the Airworthiness Directives (AD) concerning the rudder leading edge. This regulation requires modifications to the leading edge of the rudder to comply with Hawker De Havilland Technical News Sheet Beech Aust. No. 2 Issue 1 drawing 05/F/101. The regulation's jurisdictional reach is nationwide, encompassing the entire Commonwealth of Australia, and applies to all aircraft falling under the specified models, irrespective of the state or territory in which they are registered or operated. There are no stated exclusions or exemptions in the text, indicating that all relevant aircraft must comply with the directive. The regulation extends its application through subordinate instruments, which detail specific modifications and compliance timelines, ensuring adherence to the safety standards set forth by the Civil Aviation Safety Authority.

Key Provisions

The key operative sections of the Civil Aviation Regulations 1998 (Cth), specifically Part 39 - 105, focus on ensuring the airworthiness of aircraft, particularly the Beechcraft 19, 23, and 24 series aeroplanes. Section 39.105, titled "Airworthiness Directives," mandates that all models of these aircraft must comply with specific modifications. According to AD/BEECH 23/2, the leading edge of the rudder must be modified as per the Hawker De Havilland Technical News Sheet, Beech Aust. No. 2 Issue 1 drawing 05/F/101. This modification is critical for maintaining the structural integrity and safety of the aircraft. Compliance with this directive is mandatory, and the modifications must be completed before 1 September 1971. The obligations imposed by the Civil Aviation Regulations 1998 (Cth) on the parties governed by this legislation are quite clear. Operators and owners of Beechcraft 19, 23, and 24 series aeroplanes must ensure that the modifications specified in the Hawker De Havilland Technical News Sheet are carried out. This includes following the technical drawings provided in Beech Aust. No. 2 Issue 1 drawing 05/F/101. The modifications must be performed by qualified personnel who are familiar with the specific requirements of the airworthiness directive. Additionally, operators must maintain records of the modifications to demonstrate compliance with the regulations. Failure to comply with the provisions of the Civil Aviation Regulations 1998 (Cth) and the airworthiness directives can lead to serious consequences. Under section 39.105, non-compliance can result in both civil and criminal penalties. The Civil Aviation Safety Authority (CASA) has the authority to take action against operators and owners who fail to adhere to these requirements. The penalties can include fines, suspension or revocation of the aircraft's certificate of airworthiness, and in severe cases, prosecution under criminal law. The specific penalties depend on the severity and frequency of the non-compliance, but they can be significant, reflecting the importance of airworthiness and safety in aviation.