COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beagle B206 Series Aeroplanes
AD/BEA 206/5 Nose Landing Gear Spring Box 6/69
Applicability: All models fitted with Spring Box P/N AIR 47904.
Requirement: Action in accordance with Beagle SB No. B206/30 (Modification 842). Compliance: Within 200 hours time in service from 1 August 1969.
Overview
The Civil Aviation Regulations 1998 were enacted to consolidate and update the regulatory framework governing civil aviation in Australia, ensuring safety, efficiency, and environmental protection within the aviation industry. This legislative instrument, administered by the Civil Aviation Safety Authority (CASA), aims to maintain high safety standards and compliance with international aviation regulations. The regulation specifically addresses the airworthiness of aircraft, mandating that all aircraft meet stringent safety criteria to prevent accidents and ensure the safety of passengers and crew. By establishing detailed directives for maintaining aircraft airworthiness, the Civil Aviation Regulations 1998 seek to mitigate risks associated with civil aviation operations, thereby safeguarding public safety and fostering confidence in the aviation sector.
Part 39 of the Civil Aviation Regulations 1998 includes specific airworthiness directives (ADs) for various aircraft types, including the Beagle B206 Series Aeroplanes. One such directive, AD/BEA 206/5, pertains to the nose landing gear spring box and mandates compliance with Beagle Service Bulletin No. B206/30 (Modification 842). This directive applies to all Beagle B206 models fitted with Spring Box Part Number AIR 47904 and requires corrective action within 200 hours of time in service from 1 August 1969. The directive is designed to address potential safety issues related to the nose landing gear, ensuring that the aircraft remains airworthy and compliant with safety standards set by CASA. This regulation underscores the importance of regular maintenance and adherence to specific modification protocols to prevent operational hazards and maintain the integrity of the aircraft.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all operators of Beagle B206 series aeroplanes fitted with the Spring Box part number AIR 47904. This regulation mandates compliance with the Airworthiness Directive AD/BEA 206/5 concerning the nose landing gear spring box, requiring operators to take action in accordance with Beagle Service Bulletin No. B206/30 (Modification 842). The directive is applicable to all such aircraft regardless of the operator's location within Australia, thereby ensuring a uniform standard of safety across the Commonwealth. Operators must ensure that the specified modifications are implemented within 200 hours of the aircraft's time in service from 1 August 1969, or the aircraft will not be considered airworthy. This regulation does not exclude any specific entities or operations, and compliance is critical for continued airworthiness certification. The scope of the regulation may be further detailed or modified through subordinate instruments issued by the Civil Aviation Safety Authority.
Key Provisions
The key operative sections of the AD/BEA 206/5, which pertains to the nose landing gear spring box of Beagle B206 series aeroplanes, require that all models fitted with the Spring Box P/N AIR 47904 must undergo an action as specified in Beagle SB No. B206/30 (Modification 842). This directive ensures the structural integrity and safety of the nose landing gear by mandating a modification to the spring box component. Compliance with this directive is mandatory and must be achieved within 200 hours of time in service from 1 August 1969.
The Civil Aviation Safety Authority, under the Civil Aviation Regulations 1998, imposes specific obligations on the operators and owners of Beagle B206 series aeroplanes. These parties must ensure that the specified modifications are carried out by qualified personnel in accordance with the manufacturer’s instructions and the Civil Aviation Safety Authority's requirements. Operators must also maintain proper records of compliance to demonstrate that the necessary modifications have been performed within the stipulated timeframe.
Failure to comply with the provisions of AD/BEA 206/5 can result in severe consequences. The Act stipulates that non-compliance is an offence under the Civil Aviation Act 1988. The potential penalties for breaching these safety directives include significant fines and, in more serious cases, imprisonment. The specific penalties can vary depending on the nature and extent of the non-compliance, but they are designed to ensure that all aircraft meet the necessary safety standards to protect passengers and crew.
The seriousness of the penalties reflects the importance of adhering to the Airworthiness Directives issued by the Civil Aviation Safety Authority. Ensuring the structural integrity of the nose landing gear is crucial for the overall safety of the aircraft. By mandating specific modifications, the Act aims to prevent potential accidents and ensure that all aircraft operate within the highest safety standards. Non-compliance not only risks the safety of those on board but also can lead to significant legal and financial repercussions for the operators and owners involved.