COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-32 (Cherokee Six) Series Aeroplanes
AD/PA-32/16 Control Wheel Retaining Pin - Modification 8/69
Applicability: All models with S/Nos. 32-1111 to 32-1165 and S/Nos. 32-40566 to 32-40715. Document: Piper SB No. 295.
Compliance: Within 25 hours time in service after 23 July 1969.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, are fundamental in ensuring the safety and regulation of civil aviation within the country. One specific legislative instrument under these regulations is the Airworthiness Directive (AD) AD/PA-32/16, which was introduced to address the issue of control wheel retaining pin failures in Piper PA-32 (Cherokee Six) series aeroplanes. This directive was issued to ensure the airworthiness of certain models of these aircraft by mandating modifications to the control wheel retaining pin to prevent potential in-flight failures. The policy objective behind this directive is to enhance aviation safety by mitigating risks associated with the specified component, thereby protecting the lives of passengers and crew on board.
Enacted by the Parliament, the AD/PA-32/16 applies to Piper PA-32 aeroplanes with specific serial numbers, requiring compliance within 25 hours of time in service after 23 July 1969. This legislative instrument is part of a broader effort to maintain high safety standards within Australia's civil aviation sector, ensuring that all aircraft operate under stringent regulatory oversight to prevent accidents and incidents related to mechanical failures.
Scope and Application
The Civil Aviation Regulations 1998, specifically PART 39 - 105 issued by the Civil Aviation Safety Authority, includes detailed directives aimed at ensuring the airworthiness of aircraft. Among these, AD/PA-32/16 pertains to Piper PA-32 (Cherokee Six) series aeroplanes, focusing on the modification of the control wheel retaining pin. This directive applies to all models of the specified series with serial numbers falling between 32-1111 to 32-1165 and 32-40566 to 32-40715, requiring compliance within 25 hours of time in service after 23 July 1969, as detailed in Piper Service Bulletin No. 295. This regulation applies nationally across Australia, overseen by the Commonwealth, ensuring all operators and owners of the affected aircraft adhere to the stipulated modifications to maintain safety standards. There are no exclusions, exemptions, or thresholds stated within the scope of this specific directive, and its application is directly enforceable through the overarching Civil Aviation Regulations.
Key Provisions
The Civil Aviation Regulations 1998, Part 39 - 105, under the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, includes specific requirements for Piper PA-32 (Cherokee Six) series aeroplanes. The directive AD/PA-32/16 pertains to the modification of the control wheel retaining pin (section 8/69). This directive applies to all models with serial numbers (S/Nos.) ranging from 32-1111 to 32-1165 and S/Nos. 32-40566 to 32-40715. The compliance requirement necessitates that the modification be completed within 25 hours of time in service after 23 July 1969, as outlined in Piper Service Bulletin No. 295.
The obligations imposed by this directive are clear and straightforward. Operators of the specified Piper PA-32 models must ensure that the control wheel retaining pin modification is completed within the stipulated timeframe. Failure to comply with this directive may result in the aircraft being deemed non-airworthy, thus prohibiting it from operation. This requirement underscores the importance of adhering to safety standards to maintain the airworthiness of the aircraft and ensure the safety of all persons on board.
Failure to comply with the directive AD/PA-32/16 can result in significant legal and operational consequences. The Civil Aviation Regulations 1998 provide for various penalties and consequences for non-compliance. While the specific penalties are not detailed in the directive itself, general provisions of the Civil Aviation Act 1988 and the Civil Aviation Regulations 1998 may apply. These could include fines, imprisonment, or both, depending on the severity and circumstances of the breach. The primary objective of these consequences is to enforce compliance with safety regulations and to deter any actions that could compromise the safety of civil aviation operations.