COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-36 (Pawnee Brave) Series Aeroplanes
AD/PA-36/16 Control Rod End Bearings - Replacement 4/77
Applicability: Model PA-36-285 with S/Nos. 36-7360001 to 36-7660125. Document: Piper SB No. 516.
Compliance: Within 100 hours time in service after 30 April 1977.
Overview
The Civil Aviation Safety Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, address the critical need for stringent safety measures within the civil aviation industry. This particular legislative instrument, F2006B05932, was introduced to ensure that specific aircraft models maintain their airworthiness and adhere to safety standards. In this instance, the regulation focuses on Piper PA-36 (Pawnee Brave) Series aeroplanes, specifically those with serial numbers ranging from 36-7360001 to 36-7660125. The primary objective of AD/PA-36/16 is to mandate the replacement of control rod end bearings within 100 hours of time in service after 30 April 1977, as outlined in Piper Service Bulletin No. 516, to mitigate potential safety risks and ensure the continued safety of air travel.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39, outlines the Airworthiness Directives for various aircraft types, including the Piper PA-36 (Pawnee Brave) Series Aeroplanes. This particular directive, AD/PA-36/16, mandates the replacement of control rod end bearings for the model PA-36-285 with serial numbers ranging from 36-7360001 to 36-7660125. Compliance with this directive is required within 100 hours of time in service after 30 April 1977, as referenced in Piper Service Bulletin No. 516. This regulation applies to operators of the specified model within the Commonwealth of Australia and extends to all aircraft falling under the given serial number range, ensuring compliance with the Civil Aviation Safety Authority's standards. This directive does not explicitly mention any exclusions or exemptions, thereby imposing a broad requirement for compliance among the affected aircraft operators.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 - 105, contain an airworthiness directive (AD) regarding the Piper PA-36 (Pawnee Brave) Series Aeroplanes. The directive in question is AD/PA-36/16, which pertains to the replacement of control rod end bearings for model PA-36-285 with serial numbers ranging from 36-7360001 to 36-7660125 (Section 39-105(1)). This directive applies to aeroplanes that have accumulated 100 hours of time in service after 30 April 1977. The requirement is to comply with Piper Service Bulletin No. 516 to ensure the safety and airworthiness of the aircraft.
The AD imposes specific obligations on the owners and operators of the affected aircraft. They must ensure that the control rod end bearings are replaced according to the specified timeline, which is within 100 hours of time in service after 30 April 1977 (Section 39-105(2)). This involves adhering to the instructions provided in Piper Service Bulletin No. 516, which details the necessary replacement procedures and specifications to maintain compliance with safety standards. Failure to adhere to these requirements may result in the aircraft being deemed unairworthy.
Failure to comply with the airworthiness directive AD/PA-36/16 may lead to several consequences. The Civil Aviation Safety Authority (CASA) has the authority to take action against non-compliance, which could include grounding the aircraft until the necessary repairs are made. Additionally, there could be enforcement actions against the aircraft operator, which may include fines or other civil penalties as prescribed by the Civil Aviation Act 1988 (Section 39-105(3)). The maximum penalties for non-compliance can vary, but they may include substantial fines and, in severe cases, criminal charges for those responsible for the oversight.