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-32/24
Amdt 1
Main Landing Gear Torque Links - Inspection 8/79
Applicability: All models with fixed landing gear except those with torque link assembly P/N 78032-00V or later P/N.
Document: Piper SL No. 600.
Compliance: As detailed in the requirement document.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serve to regulate various aspects of civil aviation, ensuring safety and compliance within the industry. One specific legislative instrument within this framework is the Civil Aviation Safety Authority Schedule of Airworthiness Directives, which addresses various safety concerns for different aircraft models. This particular legislative instrument, F2006B05818, pertains to Piper PA-32 (Cherokee Six) Series Aeroplanes and was introduced to address safety issues related to the main landing gear torque links. The objective is to ensure that all applicable models with fixed landing gear, excluding those with specific torque link assemblies, are inspected to maintain airworthiness standards and prevent potential safety risks. The directive is designed to enforce compliance with detailed requirements as outlined in the relevant documentation, such as Piper Service Letter No. 600.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, applies to all Piper PA-32 (Cherokee Six) series aeroplanes that are subject to Australian Commonwealth aviation regulations. This legislative instrument targets specific models and mandates that all models with fixed landing gear, excluding those equipped with the torque link assembly P/N 78032-00V or later P/N, must adhere to the requirements of Airworthiness Directive AD/PA-32/24 Amendment 1, which concerns the inspection of main landing gear torque links. The scope of this directive ensures that the relevant aircraft maintain safety standards as prescribed by the Civil Aviation Safety Authority. The geographical reach of this regulation is national, affecting all aircraft operating within Australian airspace, and is enforced by the Commonwealth of Australia. The Act does not explicitly state any exclusions or exemptions, but it does delineate the specific models and components subject to the regulations. Compliance with this directive is mandatory, as outlined in the requirement document and supported by Piper Service Letter No. 600.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, mandate that certain aircraft, in this case the Piper PA-32 (Cherokee Six) series aeroplanes, must comply with Airworthiness Directives (AD) to ensure they are airworthy. One such directive, AD/PA-32/24 Amendment 1, pertains to the inspection of main landing gear torque links (section 8/79). This directive applies to all models of the Piper PA-32 series with fixed landing gear, except those equipped with the torque link assembly with part number 78032-00V or later versions. Compliance with this directive is to be achieved as detailed in the requirement document provided by Piper SL No. 600.
The AD imposes specific obligations on the operators and owners of the affected aircraft. They are required to inspect the main landing gear torque links in accordance with the specified procedures outlined in Piper SL No. 600. This inspection is crucial for ensuring the structural integrity of the landing gear and, by extension, the overall safety of the aircraft. Failure to adhere to these inspection requirements can result in the aircraft being deemed unairworthy, which could lead to grounding and potential legal ramifications.
The Civil Aviation Regulations 1998 also include provisions for penalties and consequences in the event of non-compliance with the stipulated ADs. Operators or owners who fail to adhere to the inspection requirements outlined in AD/PA-32/24 Amendment 1 may face civil penalties. The specific penalties are not detailed within the legislative instrument but are generally aligned with the Civil Aviation Act 1988, which provides for substantial fines and potential criminal charges for serious breaches. The severity of the penalties often correlates with the level of risk posed by the non-compliance to aviation safety.
In summary, the Civil Aviation Regulations 1998, through Part 39 - 105, require specific inspections on the main landing gear torque links of Piper PA-32 series aeroplanes to maintain airworthiness. Operators and owners must follow the outlined procedures and ensure compliance to avoid potential legal and financial repercussions. Non-compliance not only threatens the safety of the aircraft but also opens the door to significant penalties under aviation law.