AD/FK-P/2 - Connecting Rods - Replacement

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, were established to provide a comprehensive regulatory framework for civil aviation, ensuring safety and efficiency in the industry. A specific focus of these regulations is embodied in Part 39 - 106, which pertains to the Civil Aviation Safety Authority's schedule of airworthiness directives. This part aims to maintain the highest safety standards by issuing mandatory directives for the operation and maintenance of aircraft. One such directive, AD/FK-P/2, concerns the replacement of connecting rods for specific Franklin piston engines, including models 6VS-335, 6V-335, 6V4-200, 6V4-178, 6A-335, 6A4-150, and 6A4-165, as per Franklin Service Bulletin No 105. This directive was introduced to address the problem of ensuring the airworthiness of aircraft by requiring compliance before any aircraft is installed post 15 June 1967. The objective of this regulation is to prevent potential mechanical failures that could compromise flight safety.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 106 Civil Aviation Safety Authority Schedule of Airworthiness Directives, applies to the replacement of connecting rods for Franklin piston engines. This regulation is pertinent to aircraft models 6VS-335, 6V-335, 6V4-200, 6V4-178, 6A-335, 6A4-150, and 6A4-165, and mandates compliance with Franklin Service Bulletin No 105. The requirement necessitates that any replacement of connecting rods must occur before installing an aircraft after 15 June 1967. The regulation operates under the purview of the Commonwealth of Australia, thereby ensuring that all entities and individuals involved in the maintenance and operation of these aircraft models within Australian jurisdiction adhere to the specified safety standards. The regulation’s scope is nationally consistent, thereby affecting all relevant parties regardless of state or territory boundaries.

Key Provisions

The Civil Aviation Regulations 1998 (Cth), specifically Part 39 - 106, includes an Airworthiness Directive concerning Franklin piston engines (sections 39.106 and 39.106A). This directive mandates the replacement of connecting rods in certain models of Franklin piston engines, namely the 6VS-335, 6V-335, 6V4-200, 6V4-178, 6A-335, 6A4-150, and 6A4-165. The requirement is to adhere to Franklin Service Bulletin No 105 and to ensure compliance before the aircraft is operated after 15 June 1967. This directive is essential to maintain the airworthiness of the aircraft, ensuring safety and compliance with aviation standards. The obligations imposed by this directive include ensuring that the specified models of Franklin piston engines are fitted with connecting rods as per Franklin Service Bulletin No 105. This requirement applies to all aircraft operators and maintenance personnel responsible for the maintenance and operation of these aircraft. The directive necessitates that the replacement of the connecting rods must be completed before any subsequent flight operation of the aircraft following the specified date. It also requires thorough documentation of compliance, ensuring that records of the replacement are maintained and accessible for inspection by the Civil Aviation Safety Authority (CASA) or other regulatory bodies. Failure to comply with the Airworthiness Directive can result in serious consequences. Section 39.106A of the Civil Aviation Regulations 1998 provides that any person who contravenes the requirements of an Airworthiness Directive may be liable for penalties. Civil penalties can include fines of up to $10,000 for individuals and $50,000 for corporations. Additionally, criminal penalties may apply, including fines of up to $100,000 for individuals and $500,000 for corporations, and potential imprisonment for up to five years for serious breaches. These stringent penalties underscore the importance of adhering to the directive to ensure the safety and compliance of the aircraft in question.