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-6/16 Battery Installation - Modification N/K
Applicability: All models PC-6/340 and PC-6/350. Document: Pilatus SB No. 34.
Compliance: Before 1 November 1967.
Overview
The Civil Aviation Regulations 1998 were enacted to establish comprehensive regulations concerning civil aviation in Australia, addressing various aspects of aircraft operation, maintenance, and safety. This legislative instrument, part of the broader framework under the Civil Aviation Act 1988, aims to ensure that all civil aviation activities within Australia adhere to stringent safety standards and regulatory compliance. One specific legislative instrument within this framework, F2006B06118, targets the Pilatus Porter PC-6 Series Aeroplanes, specifically mandating modifications to the battery installation for the PC-6/340 and PC-6/350 models. This directive, issued by the Civil Aviation Safety Authority, was introduced to mitigate identified safety risks associated with the battery installation in these aircraft models, ensuring compliance with safety standards before 1 November 1967, as referenced in Pilatus SB No. 34. The policy objective behind this instrument is to enhance the overall safety of air operations by addressing potential hazards related to the aircraft's battery systems.
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 all Pilatus Porter PC-6 Series aeroplanes, including models PC-6/340 and PC-6/350. This legislation mandates compliance with modifications to the battery installation, as detailed in Pilatus Service Bulletin No. 34, and requires adherence prior to 1 November 1967. The directive is applicable to any person or entity operating these aircraft within the Commonwealth of Australia, ensuring that all modifications are implemented to maintain airworthiness standards. The regulations extend their reach nationally, applying to both state and territory jurisdictions, thereby unifying safety standards across the country. There are no specified exclusions or exemptions detailed within this directive; however, the scope of application may be further refined or expanded through subordinate instruments issued by CASA.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, establish a schedule of airworthiness directives that govern the safety of aircraft operating in Australia. Section 39.105 mentions the Pilatus Porter PC-6 Series Aeroplanes, which includes models PC-6/340 and PC-6/350. The airworthiness directive AD/PC-6/16 pertains to a modification of the battery installation. This directive is referenced in Pilatus Service Bulletin No. 34 and applies to aircraft that were in compliance before 1 November 1967.
The key provision of this directive requires that the battery installation in the affected aircraft models be modified in accordance with the specifications provided by Pilatus. This modification is intended to address safety concerns associated with the battery installation, ensuring that the aircraft can be operated safely. The directive is binding on all operators of the Pilatus Porter PC-6 Series Aeroplanes who must comply with these modifications before continuing to operate their aircraft.
Operators and owners of the affected aircraft must ensure that the modifications outlined in Pilatus Service Bulletin No. 34 are completed by qualified personnel. This includes conducting a thorough inspection of the current battery installation and implementing the required changes. Records of the modifications must be maintained and made available for inspection by the Civil Aviation Safety Authority (CASA) upon request. Failure to comply with these requirements can result in significant safety risks and potential operational restrictions for the aircraft.
Failure to comply with the airworthiness directive AD/PC-6/16 can result in enforcement actions by CASA. Under the Civil Aviation Act 1988, non-compliance may lead to penalties, including fines and the potential grounding of the affected aircraft. The maximum penalties for such breaches can be substantial, reflecting the seriousness of ensuring the airworthiness of aircraft. Additionally, operators may face civil or criminal consequences, including legal action, depending on the severity of the non-compliance and any resulting safety incidents.