COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Pilatus Porter PC-6 Series Aeroplanes
AD/PC-6/1 Rudder and Aileron Interconnection - Modification 2/66
Applicability: All models. Document: Pilatus SB No. 21. Compliance: Before 15 March 1966.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, form the foundational framework for the regulation of civil aviation within Australia. These regulations, which are administered by the Civil Aviation Safety Authority (CASA), aim to ensure the highest standards of safety and operational efficiency in the aviation industry. One particular legislative instrument, F2006B06111, pertains to Airworthiness Directives for specific aircraft models, including the Pilatus Porter PC-6 Series Aeroplanes. This legislative instrument addresses the need for mandatory modifications to the rudder and aileron interconnection of these aircraft to enhance flight safety and reliability, ensuring compliance with safety standards before a specified date. The overarching policy objective is to mitigate risks associated with flight operations by enforcing critical design modifications that have been identified as necessary to prevent potential safety hazards.
Scope and Application
The Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, specifically AD/PC-6/1, pertains to the Pilatus Porter PC-6 Series aeroplanes and mandates modifications to the rudder and aileron interconnection. This directive applies to all models within the series and necessitates compliance before 15 March 1966, as outlined in Pilatus Service Bulletin No. 21. The legislation is issued under the Civil Aviation Regulations 1998, which have a broad jurisdictional reach across the Commonwealth of Australia, governing civil aviation safety standards. The directive applies to any person or entity operating a Pilatus Porter PC-6 Series aeroplane within Australia, including both domestic and international operators as long as the aircraft is registered in Australia. The scope of the directive ensures that all such aircraft meet the specified safety requirements to maintain airworthiness. No exclusions, exemptions, or thresholds are explicitly stated in the text provided, and the directive's application can be extended or restricted through subordinate instruments issued by CASA.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, outlines the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which mandates certain modifications for Pilatus Porter PC-6 Series Aeroplanes. The directive AD/PC-6/1 pertains to the rudder and aileron interconnection, requiring modifications as detailed in Pilatus SB No. 21. This directive applies to all models of the Pilatus Porter PC-6 Series (Section 2/66). The compliance deadline for these modifications was set before 15 March 1966.
The Airworthiness Directives imposed by the Civil Aviation Regulations 1998 necessitate that owners and operators of Pilatus Porter PC-6 Series Aeroplanes must ensure that the specified modifications to the rudder and aileron interconnection are carried out. This includes adherence to the technical instructions provided in Pilatus SB No. 21, which detail the exact nature of the modifications required. Operators must complete these modifications before the specified compliance date to maintain the airworthiness of their aircraft (Section 2/66).
Failure to comply with the requirements outlined in the Airworthiness Directives may result in severe consequences. Under the Civil Aviation Regulations 1998, non-compliance with these directives can lead to significant penalties. Civil penalties may include fines and other sanctions imposed by CASA. Additionally, criminal charges may be brought against individuals or entities that fail to adhere to these safety directives, which could result in imprisonment and further financial penalties. It is essential for operators to take these directives seriously and ensure full compliance to avoid any legal repercussions (Section 2/66).
In summary, the Civil Aviation Regulations 1998 mandate specific modifications for Pilatus Porter PC-6 Series Aeroplanes concerning the rudder and aileron interconnection. Operators must adhere to the technical instructions outlined in Pilatus SB No. 21 and complete the modifications before the specified deadline. Non-compliance with these directives can lead to severe civil and criminal penalties, including fines and imprisonment. Therefore, it is crucial for all stakeholders to fully understand and comply with the requirements to ensure the continued airworthiness and safety of these aircraft (Section 2/66).