COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piaggio P166 Series Aeroplanes
AD/P166/28
Amdt 1
Applicability: All models.
Flap Control Bellcrank - Modification 7/64
Document: Replace the flap control bellcrank P/N 5313-01 with bellcrank P/N 5313.01A. Compliance: Forthwith.
Overview
The Civil Aviation Regulations 1998, as amended by the Legislative instrument F2006B05321, address the safety and maintenance requirements for aircraft operations within Australian airspace. This particular legislative instrument introduces an Airworthiness Directive concerning the Piaggio P166 Series Aeroplanes. The directive mandates the modification of the flap control bellcrank to ensure compliance with safety standards. Enacted by the Commonwealth of Australia, the objective of this legislation is to enhance the safety of civil aviation by specifying necessary modifications to critical aircraft components. The directive aims to mitigate potential safety risks associated with the identified issue, thereby protecting both the aircraft and those on board.
Scope and Application
The Civil Aviation Safety Authority (CASA) established the Civil Aviation Regulations 1998, which includes Part 39 - 105, governing the airworthiness directives for aircraft operating within Australian airspace. Specifically, AD/P166/28 Amendment 1 pertains to all models of Piaggio P166 series aeroplanes, mandating the immediate replacement of the existing flap control bellcrank part number 5313-01 with the modified bellcrank part number 5313.01A to ensure compliance with airworthiness standards. This directive applies to any person or entity operating such aircraft in Australia, extending its jurisdictional reach across the Commonwealth, and it does not include any specific exclusions or thresholds beyond the requirement for immediate compliance. The regulation’s scope is further extended and detailed through subordinate instruments, which provide additional specifications and enforcement mechanisms.
Key Provisions
The main operative sections of the Civil Aviation Regulations 1998, specifically Part 39 - 105, include the Schedule of Airworthiness Directives which detail modifications and compliance requirements for specific aircraft models. In this case, AD/P166/28 Amendment 1 pertains to the Piaggio P166 Series Aeroplanes, addressing the flap control bellcrank modification (sections 39.105). The directive requires that the existing flap control bellcrank P/N 5313-01 be replaced with the new bellcrank P/N 5313.01A, with compliance to be carried out forthwith.
The obligations imposed by this directive are clear and direct. Operators of Piaggio P166 Series Aeroplanes must ensure that the specified modification is completed without delay. This involves the replacement of the existing flap control bellcrank with the new version, ensuring that the aircraft meets the updated safety standards set by the Civil Aviation Safety Authority (CASA). Failure to comply with this directive could result in the aircraft being deemed non-airworthy, which in turn could prevent it from being operated legally.
In terms of consequences for non-compliance, the regulations are stringent. Any breach of the airworthiness directive could lead to enforcement actions by CASA. This may include penalties such as fines, suspension of the aircraft's certificate of airworthiness, or other regulatory sanctions. While the specific penalties are not detailed within this particular directive, it is known that non-compliance with airworthiness directives can result in significant legal and financial repercussions for operators. The overarching aim is to ensure that all aircraft meet the highest safety standards, thereby protecting the safety of all passengers and crew.