AD/PA-32/54 Amdt 2 - Oil Coolers - Inspection and Replacement

Overview

The Civil Aviation Regulations 1998, as amended, were enacted to provide comprehensive regulations for civil aviation in Australia, addressing various aspects of safety, licensing, and operational standards. This legislative framework was developed to ensure the safety and efficiency of air travel within the country, aligning with international standards and practices. Specifically, the regulations govern the issuance and management of airworthiness certificates, pilot licensing, and the maintenance of aircraft to ensure that they meet required safety standards. The regulations were introduced by the Commonwealth Parliament to fill a critical gap in the regulatory oversight of civil aviation activities in Australia, aiming to protect public safety and maintain the integrity of the nation’s aviation infrastructure. One specific legislative instrument under the Civil Aviation Regulations 1998 is the Airworthiness Directive AD/PA-32/54 Amendment 2, which pertains to the inspection and replacement of oil coolers in Piper PA-32 (Cherokee Six) Series Aeroplanes. This directive was introduced to address identified safety issues related to the oil coolers in these aircraft models, ensuring they meet required safety standards and preventing potential failures that could compromise flight safety. The policy objective of this directive is to enhance the operational safety of the specified aircraft models by mandating regular inspections and necessary replacements of oil coolers, thereby reducing the risk of engine failure and associated hazards.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives for Piper PA-32 (Cherokee Six) Series Aeroplanes, applies to certain series of Piper PA-32R-300 and PA-32RT-300 models, identified by their serial numbers. The regulation mandates compliance with the airworthiness directives set forth in Piper SB No. 586B, which includes detailed requirements for oil cooler inspection and replacement. This regulation applies to the specified serial number ranges and is applicable across the Commonwealth of Australia under the jurisdiction of the Civil Aviation Safety Authority. The regulation does not explicitly state any exclusions or exemptions but implies compliance is mandatory for the specified aircraft within the stated serial number ranges. The application of this regulation may be further extended or specified through subordinate instruments or additional guidance issued by the Civil Aviation Safety Authority.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, includes specific airworthiness directives for various aircraft, including the Piper PA-32 (Cherokee Six) series aeroplanes. Specifically, AD/PA-32/54 Amendment 2 mandates inspections and potential replacements of oil coolers for certain models. This directive applies to the PA-32R-300 series with serial numbers ranging from 32R-7680001 to 32R-7880068 and the PA-32RT-300 series with serial numbers from 32R-7885001 to 32R-7885207 (Section 10/78). Compliance with these directives is outlined in Piper Service Bulletin No. 586B, with specific requirements for Parts 1 and 2. Part 1 of the requirement document specifies detailed inspection procedures, which can be performed by the pilot in command without the need for certification, whereas Part 2 mandates these inspections to be completed before 31 August 1979. The obligations imposed by these airworthiness directives include thorough inspections of the oil coolers to ensure they meet specified standards. Operators of the affected aircraft must adhere to the guidelines provided in Piper SB No. 586B, ensuring that the inspections are conducted meticulously and that any necessary replacements are performed correctly. The responsibility lies with the aircraft owner or operator to ensure compliance with these directives, which are critical for maintaining the airworthiness of the aircraft. Failure to comply with these airworthiness directives can result in serious consequences. While the specific penalties are not detailed in the provided text, non-compliance with airworthiness directives generally can lead to significant civil and criminal penalties. Such penalties may include fines, suspension or revocation of aircraft operating certificates, and potential criminal charges against individuals responsible for the non-compliance. The exact penalties can vary based on the severity of the breach and the specific regulations breached, but they are intended to enforce the stringent safety standards required in civil aviation.