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 121/19 Rudder Pedal Anchorages 12/77
Applicability: All models.
Requirement: Action in accordance with Beagle SB No. B121/73. Compliance: Within 100 hours time in service after 31 December 1977.
Overview
The Civil Aviation Regulations 1998 (the Regulations), administered by the Civil Aviation Safety Authority (CASA), were enacted by the Parliament of Australia to provide a comprehensive framework for ensuring the safety of civil aviation within Australia. One specific aspect of the Regulations is addressed in Part 39, which includes Airworthiness Directives (ADs) intended to maintain and enhance aircraft safety. AD/BEA 121/19, issued under the authority of the Civil Aviation (Airworthiness of Aircraft) Regulations 1998, is one such directive aimed at ensuring the safety of Beagle B121 (Pup) series aeroplanes by mandating the inspection and repair of rudder pedal anchorages. The policy objective behind this directive is to prevent structural failures that could potentially compromise the safety and control of the aircraft, thereby protecting the lives of passengers and crew, as well as reducing the risk of accidents associated with rudder pedal detachment.
Scope and Application
The Civil Aviation Safety Authority (CASA) under the Civil Aviation Regulations 1998 applies specific Airworthiness Directives (AD) to ensure the safety and airworthiness of aircraft. Part 39 - 105 of these regulations includes AD/BEA 121/19, which pertains to rudder pedal anchorages of Beagle B121 (Pup) series aeroplanes. This directive applies to all models within this series and mandates that action must be taken in accordance with Beagle Service Bulletin No. B121/73. Compliance with this directive is required within 100 hours of time in service after 31 December 1977. The directive encompasses the entire range of Beagle B121 aeroplanes and sets a clear timeframe for compliance, ensuring that all such aircraft meet specified safety standards. The Civil Aviation Regulations 1998, through the Airworthiness Directives, extend their jurisdiction over all civil aviation activities within Australia, thereby enforcing safety compliance on a national level.
Key Provisions
The primary operative sections of the Civil Aviation Regulations 1998, PART 39 - 105, specifically AD/BEA 121/19, concern the maintenance and safety directives for Beagle B121 (Pup) series aeroplanes, particularly focusing on rudder pedal anchorages. Section 12/77 dictates that all models of these aeroplanes must comply with the action outlined in Beagle Service Bulletin No. B121/73. The compliance requirement stipulates that these actions must be completed within 100 hours of time in service after 31 December 1977.
The Act imposes clear obligations on the operators and owners of Beagle B121 (Pup) series aeroplanes to ensure that the specified maintenance actions are carried out as detailed in the Service Bulletin. This includes conducting thorough inspections and necessary repairs or modifications to the rudder pedal anchorages to meet the safety standards set forth by the Civil Aviation Safety Authority (CASA). Operators must maintain detailed records of these compliance actions to demonstrate adherence to the directive.
Failure to comply with the provisions outlined in AD/BEA 121/19 can lead to serious civil and criminal consequences. Specifically, non-compliance may result in the aeroplane being deemed unairworthy, potentially leading to fines or other regulatory penalties under the Civil Aviation Act 1988. The maximum penalties for such breaches can include substantial fines and, in severe cases, imprisonment for directors of companies found guilty of repeated or wilful violations. Additionally, CASA may take enforcement actions such as grounding the aircraft until the required maintenance is performed, which can significantly impact the operational viability of the aeroplane.