AD/AL 60/7 Amdt 1 - Capacitor Fastening - Modification

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, serve as a comprehensive framework to ensure the safety and efficiency of civil aviation within Australia. Specifically, Part 39 - 105 of the Civil Aviation Regulations 1998 addresses the authority and procedures for issuing airworthiness directives, which are regulatory mandates designed to address safety issues identified in aircraft. This part was introduced to fill a critical gap in ensuring that all civil aircraft operating in Australian airspace meet the highest safety standards. The policy objective of these regulations is to maintain a robust and proactive approach to aviation safety, thereby protecting the public and maintaining the integrity of the civil aviation system. The Civil Aviation Regulations 1998 empower the Civil Aviation Safety Authority (CASA) to issue airworthiness directives to address specific safety concerns. One such directive, AD/AL 60/7 Amendment 1, pertains to the Aermacchi - Lockheed AL 60 Series Aeroplanes, focusing on the modification of capacitor fastening as outlined in Aermacchi Lockheed 60 Mod. Bulletin No. 16. This directive mandates compliance before 1 September 1971, underscoring the urgency and importance of addressing the identified safety issue. The overarching goal is to ensure that all aircraft meet stringent safety standards, thereby mitigating risks and enhancing the overall safety of civil aviation.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority’s Schedule of Airworthiness Directives, and in this instance, it applies to Aermacchi - Lockheed AL 60 Series Aeroplanes. This legislation mandates the compliance with Airworthiness Directive AD/AL 60/7 Amendment 1, which addresses capacitor fastening modifications as outlined in Aermacchi Lockheed 60 Modification Bulletin No. 16. The requirement for compliance with this directive must be met prior to 1 September 1971, ensuring that all relevant aircraft meet the specified airworthiness standards. This regulation applies to all persons and entities operating Aermacchi - Lockheed AL 60 Series Aeroplanes within the jurisdiction of the Commonwealth of Australia, and its enforcement is overseen by the Civil Aviation Safety Authority. The scope of this directive is specifically tailored to ensure the safety and airworthiness of the mentioned aircraft models, with no exclusions or exemptions detailed within the provided text. The application of this regulation is not extended or restricted through subordinate instruments in the provided excerpt.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives. This particular directive, AD/AL 60/7 Amendment 1, focuses on the modification of capacitor fastening for Aermacchi - Lockheed AL 60 Series Aeroplanes. The applicability of this directive is detailed in the requirement document, specifically Aermacchi Lockheed 60 Mod. Bulletin No. 16, which outlines the scope and specifics of the modification required. Compliance with these directives must be achieved before 1 September 1971, as stipulated by the regulation. The key operative sections of this directive include the identification of the affected aircraft models, the specific modification required, and the timeframe within which compliance must be achieved. Section 39.105 details the general obligations under the CASA's airworthiness directives, while the specific requirements for this directive are outlined in the referenced bulletin. These requirements mandate that the capacitor fastening on the Aermacchi - Lockheed AL 60 Series Aeroplanes be modified to meet the specified standards to ensure the safety and airworthiness of the aircraft. The obligations imposed by this Act on the parties or entities it governs include ensuring that the modifications are correctly implemented and documented. Aircraft operators and owners must adhere to the detailed instructions provided in the requirement document, ensuring that all capacitor fastenings are modified as specified by the bulletin. This includes thorough inspection, modification, and certification processes to confirm that the aircraft meets the airworthiness criteria set by CASA. Failure to comply with these obligations can result in serious consequences, including the potential grounding of the aircraft and other enforcement actions by CASA. The consequences for non-compliance with the provisions of this directive are significant. Section 39.105 specifies that failure to comply with an airworthiness directive can result in civil or criminal penalties. The maximum penalties for non-compliance can include substantial fines and, in severe cases, imprisonment. Additionally, aircraft found to be non-compliant may be grounded, preventing them from being operated until the required modifications are completed and certified as compliant. This not only poses financial and operational risks to the aircraft operators but also compromises the safety of passengers and crew. Therefore, it is crucial for all parties involved to adhere strictly to the requirements set forth in the directive.