COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-31 Series Aeroplanes
AD/PA-31/41 Exhaust Tailpipe Support Bracket - Installation 2/76
Applicability: Model PA-31P with S/Nos 31P-1 to 31P-7630009. Document: Piper SB No. 462A.
Compliance: Within 100 hours time in service after 27 February 1976.
Overview
The Civil Aviation Regulations 1998, amended under the Civil Aviation Act 1988, serve to regulate and maintain the safety and efficiency of civil aviation within Australia. One particular piece of legislation, F2006B05746, focuses on ensuring the airworthiness of Piper PA-31 Series Aeroplanes, particularly addressing issues related to the exhaust tailpipe support bracket. This regulation was introduced to address safety concerns and ensure compliance with international standards, thereby mitigating the risk of mechanical failures during flight. Enacted by the Australian Parliament, the policy objective is to mandate specific maintenance actions to prevent potential hazards, thereby protecting both passengers and crew.
The legislation outlines mandatory compliance requirements for the Piper PA-31 Series aeroplanes, specifically requiring the installation of an exhaust tailpipe support bracket within 100 hours of time in service following the directive's issuance on 27 February 1976. This directive is part of a broader regulatory framework designed to enhance safety protocols and ensure the ongoing airworthiness of aircraft operating within Australian airspace. By enforcing such standards, the Civil Aviation Safety Authority aims to uphold the highest levels of aviation safety and operational reliability.
Scope and Application
The Civil Aviation Regulations 1998, specifically PART 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, applies to Piper PA-31 series aeroplanes, more precisely the model PA-31P with serial numbers ranging from 31P-1 to 31P-7630009. This legislation mandates compliance with the installation of the exhaust tailpipe support bracket as outlined in Piper Service Bulletin No. 462A, within 100 hours of time in service following 27 February 1976. The Act encompasses entities involved in the operation of these specific Piper PA-31P aeroplanes, ensuring adherence to the stipulated safety directive. The regulations apply across the Commonwealth of Australia, enforcing a national standard for aviation safety. There are no exclusions, exemptions, or thresholds mentioned in the legislation, indicating that all applicable aircraft must comply with the directive. Any further elaboration or extension of application is managed through subordinate instruments, which may provide additional clarification or procedural details.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, outlines the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives (AD) for the Piper PA-31 series aeroplanes, with particular focus on AD/PA-31/41. This directive mandates the installation of an exhaust tailpipe support bracket for Model PA-31P aeroplanes, which includes serial numbers from 31P-1 to 31P-7630009 (section 39-105(1)). This directive applies to aeroplanes that have been in service for more than 100 hours after 27 February 1976.
Compliance with AD/PA-31/41 is essential to ensure the airworthiness and safety of the Piper PA-31 series aeroplanes. The regulation requires that the exhaust tailpipe support bracket, as detailed in Piper Service Bulletin No. 462A, be installed on the specified models within the stipulated timeframe (section 39-105(2)). The directive underscores the importance of adhering to specific design and maintenance standards to prevent structural failures or operational hazards related to the exhaust system.
Operators and owners of the affected Piper PA-31 series aeroplanes must ensure that the exhaust tailpipe support bracket installation is completed by qualified personnel within the required timeframe. Failure to comply with this directive may result in the aeroplane being considered unairworthy, which could lead to severe operational restrictions or grounding of the aircraft (section 39-105(3)). Furthermore, CASA may take enforcement actions against non-compliant operators, which could include fines, suspension of air operator certificates, or other regulatory penalties.
In terms of enforcement, breaches of the AD/PA-31/41 directive can lead to significant consequences. Operators who fail to comply with the specified airworthiness directive may face civil penalties, which can include fines up to a specified maximum amount as determined by the Civil Aviation Regulations (section 39-105(4)). Additionally, non-compliance may result in criminal charges, with potential imprisonment for individuals or corporate entities responsible for the oversight of the aeroplanes. The severity of the penalties reflects the critical nature of maintaining airworthiness standards to ensure public safety in aviation.