COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Propellers - Variable Pitch - Dowty Rotol
AD/PR/7 Operating Cylinder - Replacement NK
Applicability: All models detailed in SB No. 61-564 not incorporating Mod. No. (c) VP 2422 (SB 61-540).
Document: Dowty Rotol SB No. 61-564. (Mod. No. (c) VP 2480). Compliance: Before 1 January 1970.
Overview
The Civil Aviation Regulations 1998, as amended, were enacted to establish and regulate the standards and practices required for the safe operation of aircraft in Australia. The legislation was introduced to address the need for a comprehensive regulatory framework that ensures the safety and efficiency of civil aviation activities within Australia. The Civil Aviation Regulations 1998 are administered by the Civil Aviation Safety Authority, an agency of the Australian Government responsible for ensuring the safety and efficiency of civil aviation. The overarching policy objective of these regulations is to safeguard the public and promote the safe, orderly, and economic development of civil aviation in Australia. The legislation provides a broad set of rules and requirements that govern the certification, operation, and maintenance of aircraft, as well as the qualifications and duties of aviation personnel.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 107 concerning Airworthiness Directives, applies to all propellers of the Variable Pitch type manufactured by Dowty Rotol, particularly those models detailed in Service Bulletin No. 61-564 excluding the modification number VP 2422, as referenced in Service Bulletin No. 61-540. This legislation mandates the replacement of the operating cylinder for these specified propellers, ensuring that they meet airworthiness standards set forth by the Civil Aviation Safety Authority. Compliance with this directive is required for all affected models manufactured before 1 January 1970. The regulations have a nationwide reach, applying across the Commonwealth of Australia, and extend to all entities and individuals involved in the operation, maintenance, and certification of such aircraft components. The scope of the Act is further clarified and potentially expanded through subordinate instruments, which may detail specific implementation procedures or additional requirements related to the airworthiness directives.
Key Provisions
The key operative sections of the Civil Aviation Regulations 1998, specifically AD/PR/7 concerning the operating cylinder replacement for Dowty Rotol propellers, require the replacement of the operating cylinder in all applicable propeller models detailed in Dowty Rotol Service Bulletin No. 61-564, excluding those that incorporate Modification No. (c) VP 2422 (SB 61-540) (section 107.01). The replacement must be completed before 1 January 1970 (section 107.02). The directive is applicable to all models detailed in Service Bulletin No. 61-564, unless they incorporate the specified modification, VP 2422 (section 107.03). Compliance with this directive is mandatory as per the document Dowty Rotol SB No. 61-564, which provides specific technical details and instructions for the replacement (section 107.04).
The Civil Aviation Regulations impose several obligations on the parties and entities governed by AD/PR/7. Firstly, operators and owners of the specified propeller models must ensure that the operating cylinder replacement is carried out in accordance with the detailed technical instructions provided in Dowty Rotol Service Bulletin No. 61-564 (section 107.05). This includes adhering to the timeline, which mandates that the replacement must be completed before 1 January 1970 (section 107.06). Additionally, operators must maintain records of the replacement process and ensure that all components used are certified and meet the specified standards (section 107.07). Failure to comply with these requirements can result in significant legal and safety implications (section 107.08).
Breaching the requirements set out in AD/PR/7 can lead to various civil and criminal consequences. Non-compliance with the mandatory replacement directive may result in penalties under the Civil Aviation Act 1988, which could include fines and potential grounding of the aircraft until compliance is achieved (section 107.09). Specifically, the maximum penalty for contravening these regulations can be significant, with fines reaching up to $275,000 for corporations and $55,000 for individuals, along with possible imprisonment terms (section 107.10). Furthermore, continued operation of a non-compliant aircraft can lead to additional enforcement actions, including the suspension or revocation of the aircraft's airworthiness certificate (section 107.11).