Overview

The Civil Aviation Regulations 1998, as amended, form a comprehensive regulatory framework governing civil aviation in Australia. Specifically, Part 39 - 105 of these regulations addresses the issuance of Airworthiness Directives (ADs) by the Civil Aviation Safety Authority (CASA), which is the body responsible for enforcing and overseeing compliance with civil aviation safety standards. One such AD, F2006B06150, was introduced to address potential safety issues related to the aileron mass balance weights and Flettner tabs on Pilatus Porter PC-6 series aeroplanes, specifically those up to and including Manufacturing Serial Number (MSN) 939. The directive was issued to ensure that these aircraft conform to the specifications outlined in Pilatus Service Bulletins No. 57-001 and No. 62B, aiming to rectify any incorrect configurations and the use of unapproved parts that could compromise the safety of the aircraft. This AD became effective on 16 May 2002, requiring compliance before 16 June 2002.

Scope and Application

The Civil Aviation Regulations 1998 (CAR 1998) govern the safety standards and operational requirements for civil aviation within Australia, ensuring the protection of the public and the maintenance of safety in the aviation sector. Specifically, Part 39 - 105 pertains to Airworthiness Directives (ADs) issued by the Civil Aviation Safety Authority (CASA) to address identified safety issues. An example of such an AD is AD/PC-6/46, which applies to all Pilatus Porter PC-6 series aeroplanes up to and including Manufacturer Serial Number (MSN) 939. The AD mandates corrective actions to rectify unsafe conditions related to aileron mass balance weights and Flettner tabs, requiring compliance with specified instructions from Pilatus Service Bulletins No. 57-001 and No. 62B. The directive became effective on 16 May 2002 and required compliance before 16 June 2002, unless the actions had already been completed. The AD's scope is geographically confined to the Commonwealth of Australia, with its enforcement managed by CASA, ensuring that the specified aircraft meet the required safety standards.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, contain specific provisions for Airworthiness Directives (AD) issued by the Civil Aviation Safety Authority (CASA). Section 39.1 (1) empowers a CASA delegate to issue such directives when they identify an unsafe condition with a particular type of aircraft or aeronautical product. In this instance, the AD issued is AD/PC-6/46, concerning the Pilatus Porter PC-6 Series Aeroplanes. This particular AD mandates actions to address issues with aileron mass balance weights and Flettner tabs, as outlined in the requirement section. It specifies that these actions must be in accordance with the Accomplishment Instructions of Pilatus PC-6 Service Bulletin No. 57-001, dated 20 December 2001, and applicable portions of Pilatus PC-6 Service Bulletin No. 62B. The AD applies to all PC-6 series aircraft up to and including MSN 939. The directive requires the necessary corrective actions to be completed before 16 June 2002, unless the actions have already been performed. The directive became effective on 16 May 2002. The directive mandates compliance with the Accomplishment Instructions of Pilatus PC-6 Service Bulletin No. 57-001 and relevant parts of Service Bulletin No. 62B. Additionally, it references a Swiss FOCA AD, HB 2002-001, indicating international coordination in addressing the identified safety issue. The AD imposes obligations on aircraft operators and maintenance personnel to ensure that the specified corrective actions are taken on the applicable aircraft. This includes verifying the configuration of aileron mass balance weights and Flettner tabs, and ensuring that any parts installed are approved and comply with original manufacturer’s specifications. Failure to adhere to the AD can result in serious safety risks, as incorrect configurations or the use of unapproved parts may lead to unsafe conditions. The AD is backed by regulatory authority, and non-compliance may result in enforcement actions under the Civil Aviation Act 1988. Breach of the requirements stipulated in this AD may lead to significant legal and safety consequences. The Civil Aviation Act 1988 and associated regulations provide for both civil and criminal penalties for non-compliance with ADs. Civil penalties can include fines up to $126,000 for individuals and $630,000 for corporations, as per section 364 of the Act. Criminal penalties may also apply, with maximum fines of up to $504,000 for individuals and $2,520,000 for corporations, as well as potential imprisonment terms. These severe penalties underscore the importance of strict compliance with ADs to ensure aviation safety.