COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Pitts S-1 and S-2 Series Aeroplanes
AD/PITTS S-2/2 Aileron Inter-Connect Tube - Modification 8/73
Applicability: Model S-2A with S/Nos. 2001 to 2025. Document: Pitts SB No. 5; Supplement No. 1.
Compliance: Before 30 September 1973 unless already accomplished.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, address the critical need for maintaining the highest safety standards within the civil aviation sector. This legislative instrument is designed to ensure the airworthiness of aircraft operating within Australia, with a particular focus on specific aircraft models and their compliance with safety directives. One such directive, AD/PITTS S-2/2, pertains to the Pitts S-1 and S-2 series aeroplanes and mandates modifications to the aileron inter-connect tube. This directive is aimed at addressing potential safety issues by ensuring that the specified models adhere to the required safety standards before a certain compliance deadline. The overarching policy objective of these regulations is to mitigate risks and enhance the safety of civil aviation operations within Australia.
The Pitts S-2 series aeroplanes, specifically those with serial numbers 2001 to 2025, are required to undergo a modification to the aileron inter-connect tube as stipulated in the AD/PITTS S-2/2 directive. This requirement must be fulfilled before 30 September 1973 unless the modification has already been completed. This directive is part of a broader schedule of airworthiness directives aimed at ensuring that all civil aircraft operate within safe parameters. By mandating specific modifications and compliance deadlines, the Civil Aviation Regulations 1998 work to uphold stringent safety standards, thereby protecting both the flying public and aviation personnel.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39, applies specifically to the Pitts S-1 and S-2 series aeroplanes, more precisely to the Pitts S-2A model with serial numbers ranging from 2001 to 2025. This directive mandates a modification to the aileron inter-connect tube, which must be implemented before 30 September 1973 for those aircraft that have not already undergone the specified modification. The directive is enforceable by the Civil Aviation Safety Authority, ensuring adherence to the outlined safety standards and specifications. The geographic and jurisdictional reach of this legislation is national, applying across the Commonwealth of Australia, thereby impacting all relevant aircraft within the defined model and serial number range, regardless of where they are operated within the country. The Act does not provide for any exclusions, exemptions, or thresholds other than the specific compliance deadline and the model and serial number specifications. Any further application or clarification of these directives may be extended through subordinate instruments or additional documentation, such as Pitts SB No. 5; Supplement No. 1, which provides detailed instructions for compliance.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates modifications to the Pitts S-1 and S-2 series aeroplanes through the Airworthiness Directive AD/PITTS S-2/2. This directive targets the aileron inter-connect tube of model S-2A aircraft with serial numbers (S/Nos.) ranging from 2001 to 2025. The requirement stems from document Pitts SB No. 5; Supplement No. 1 and must be complied with before 30 September 1973, unless the modification has already been completed. This directive ensures the structural integrity and safety of the aircraft by specifying necessary changes to the aileron system.
The Civil Aviation Regulations impose several obligations on the parties or entities governed by this Act. Owners and operators of the affected Pitts S-2A aeroplanes must ensure that the modifications to the aileron inter-connect tube are carried out by authorised personnel in accordance with the specifications outlined in Pitts SB No. 5; Supplement No. 1. Additionally, compliance must be achieved before the specified deadline to maintain the airworthiness of the aircraft. Failure to adhere to these requirements could result in the aircraft being deemed unairworthy, thereby affecting its ability to operate legally within Australian airspace.
Breach of the obligations stipulated in the Civil Aviation Regulations, particularly those outlined in the Airworthiness Directive AD/PITTS S-2/2, may lead to various legal consequences. If an aircraft is found to be non-compliant with the specified modifications, the operator could face enforcement actions from the Civil Aviation Safety Authority (CASA). The penalties for non-compliance can be significant and may include fines, suspension or revocation of the aircraft’s certificate of airworthiness, or other regulatory sanctions. The exact penalties are not specified in the legislative instrument but can be severe, reflecting the importance of adhering to air safety regulations to protect public safety and ensure compliance with civil aviation standards.