COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-28 Series Aeroplanes
AD/PA-28/49 Air Conditioning System - Modification 10/74
Applicability: All the following models when fitted with factory installed air conditioning systems: Model PA-28-140 with S/Nos. 28-250001, 28-7125472 to 28-7425343,
Model PA-28- 180 with S/Nos. 28-5653, 28-7205092 to 28-7405188. Model PA-28R-200 with S/Nos. 28R-8235001 to 28R-7435255.
Document: Piper SB No. 427.
Compliance: Within 100 hours time in service after 31 October 1974.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, are a comprehensive set of rules governing civil aviation within the country. One specific legislative instrument, F2006B05607, pertains to Part 39 - 105, which details the Civil Aviation Safety Authority's Schedule of Airworthiness Directives. This particular directive, AD/PA-28/49, targets Piper PA-28 series aeroplanes equipped with factory-installed air conditioning systems, specifically addressing models PA-28-140, PA-28-180, and PA-28R-200 within certain serial number ranges. The directive mandates modifications to the air conditioning system to enhance safety and compliance with civil aviation standards, aiming to mitigate any potential risks associated with the specified models. The directive was issued to ensure that these aircraft meet the necessary safety requirements, thereby protecting both the aircrew and passengers.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to airworthiness directives issued by the Civil Aviation Safety Authority (CASA) and applies to certain Piper PA-28 Series aeroplanes when they are fitted with factory-installed air conditioning systems. This legislative instrument targets specific models and serial numbers of the Piper PA-28 aeroplanes, including the PA-28-140, PA-28-180, and PA-28R-200 models, with particular serial number ranges. The directive mandates compliance within 100 hours of time in service after 31 October 1974, ensuring that modifications to the air conditioning system are undertaken to maintain the safety and airworthiness of these aircraft. The regulation is enforceable across the Commonwealth of Australia, and its scope is limited to the specified models and serial numbers of the Piper PA-28 Series aeroplanes, with no stated exclusions or exemptions within the provided text. The directive extends its application through the requirement to comply with Piper Service Bulletin No. 427, which likely outlines the specific modifications to be made.
Key Provisions
The main operative sections of the Civil Aviation Regulations 1998, Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, specifically AD/PA-28/49, concern the air conditioning systems of certain Piper PA-28 series aeroplanes. Section 10/74 addresses the applicability of these directives to specific models and serial numbers of the PA-28-140, PA-28-180, and PA-28R-200 series when they are fitted with factory-installed air conditioning systems. Compliance is mandated within 100 hours of time in service after 31 October 1974.
The Act imposes several obligations on the parties or entities it governs. Firstly, it requires aircraft owners and operators to ensure that any Piper PA-28 series aeroplanes within the specified serial numbers and models comply with the airworthiness directive AD/PA-28/49. This involves implementing the necessary modifications to the air conditioning systems as outlined in Piper SB No. 427 within the stipulated timeframe. Failure to comply may result in the aircraft being deemed unairworthy and subject to grounding or other enforcement actions.
Additionally, the Act mandates that any modifications or repairs must be performed by authorised personnel who are qualified and experienced in working on these specific aircraft models. Records of the compliance actions taken must be maintained and made available for inspection by the Civil Aviation Safety Authority (CASA). These records should include details of the modifications, the personnel involved, and the dates on which the work was performed.
The Civil Aviation Regulations 1998 also establish specific offences and penalties for non-compliance with the airworthiness directives. Section 91.209 of the Act provides that any person who operates an aircraft in a manner that contravenes the airworthiness requirements is liable to penalties. The maximum penalty for such an offence can include fines of up to $150,000 for individuals and $750,000 for corporations, as well as potential imprisonment terms. Furthermore, CASA may impose further administrative penalties, such as suspension or revocation of the aircraft's certificate of airworthiness, which can have significant operational and financial repercussions for the non-compliant party.