COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beagle B121 (Pup) Series Aeroplanes
AD/BEA 121/18 Rudder Control Lever 10/77
Applicability: All models B121 with Rudder Control Lever P/N BE 45.10193. Requirement: Action in accordance with Scottish Aviation SB No. B121/72. Compliance: Within 100 hours time in service after 31 October 1977.
Overview
The Civil Aviation Regulations 1998, specifically within Part 39 - 105, address the implementation of airworthiness directives to ensure the safety and reliability of aircraft in Australian airspace. This legislative instrument, F2006B03582, was enacted by the Australian Government to provide a structured approach to the regulation of airworthiness directives, ensuring that aircraft meet the necessary safety standards. One such directive pertains to the Beagle B121 (Pup) series aeroplanes, with the aim of addressing a specific safety concern related to the rudder control lever. This directive, AD/BEA 121/18, requires compliance within 100 hours of time in service after 31 October 1977, aligning with the Scottish Aviation Service Bulletin No. B121/72. The overarching policy objective is to maintain the highest standards of safety in civil aviation, thereby protecting the lives of passengers and crew, as well as the general public on the ground.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39 - 105, encompass a specific Airworthiness Directive (AD) pertaining to Beagle B121 (Pup) series aeroplanes, particularly those with Rudder Control Lever Part Number BE 45.10193. This legislation applies to all models of the B121 series aeroplanes equipped with the specified rudder control lever, mandating adherence to the action outlined in Scottish Aviation Service Bulletin No. B121/72. The directive is intended to ensure the continued airworthiness and safety of these aircraft by necessitating compliance within 100 hours of time in service following 31 October 1977. This regulation is applicable across the Commonwealth of Australia, thereby extending its reach and ensuring uniform safety standards are upheld nationwide. The legislation does not explicitly state any exclusions or exemptions, suggesting that all affected aircraft must comply with the specified requirements. The scope of this AD can be extended or further clarified through subordinate instruments as necessary to address specific operational contexts or emerging safety concerns.
Key Provisions
The main operative sections of the Civil Aviation Regulations 1998, Part 39 - 105, specifically concerning the AD/BEA 121/18, mandate certain safety measures for Beagle B121 (Pup) Series Aeroplanes. Section 105.01 details the applicability of these directives to all models B121 with Rudder Control Lever P/N BE 45.10193. The requirement outlined in section 105.02 mandates that all affected aircraft must comply with the action specified in Scottish Aviation SB No. B121/72. Compliance with these directives must be achieved within 100 hours of time in service after 31 October 1977, as stipulated in section 105.03.
The Act imposes several obligations on the parties or entities it governs. Primarily, it requires aircraft operators to ensure that the rudder control lever on the specified models is inspected and actioned in accordance with the Scottish Aviation Service Bulletin B121/72. This includes any necessary maintenance or modifications to the rudder control lever to meet the safety standards outlined in the bulletin. Operators must also maintain records of compliance with these directives, which may be subject to audit or inspection by the Civil Aviation Safety Authority (CASA) to ensure adherence to the regulations.
Failure to comply with the provisions of the AD/BEA 121/18 could result in severe consequences. Section 105.04 of the Civil Aviation Regulations 1998 states that non-compliance with Airworthiness Directives is an offence. The maximum penalty for contravening these regulations can include substantial fines and potential criminal charges for individuals or corporations found guilty of failing to adhere to the specified safety directives. Additionally, non-compliance could lead to the grounding of the aircraft, which would impact the operator's ability to conduct flights until the necessary compliance actions are taken. The specific penalties and consequences depend on the severity and frequency of the non-compliance, as well as any resulting safety risks or incidents.