COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Airparts (NZ) Ltd. FU 24 Series Aeroplanes
AD/FU24/41 Pilot Restraint Installation - Modification 9/71
Applicability: All models in agricultural category not modified in accordance with the provisions of Supplemental Type Certificate 61-1, or equivalent approved schemes, which permit the use of a fixed type safety harness.
Requirement: Modify the safety harness installation by fitting a multidirectional type inertia reel complying with Specification IL-R-8236 Type MA2-MA4 or -MA6, or such other specification which is acceptable to the Secretary.
Compliance: Within 6 months after 30 September 1971.
Overview
The Civil Aviation Regulations 1998, which were enacted by the Australian Parliament, form a fundamental part of the regulatory framework for civil aviation safety in Australia. These regulations, including Part 39 - 105 concerning Airworthiness Directives, are designed to ensure that all civil aircraft operated within Australia meet the necessary safety standards. One such directive, AD/FU24/41, pertains to the installation of pilot restraints in FU 24 Series Aeroplanes manufactured by Airparts (NZ) Ltd. This directive was introduced to address the safety gap associated with the lack of adequate pilot restraint systems in certain models, aiming to reduce the risk of injury or fatality in the event of an in-flight emergency. The policy objective behind this directive is to mandate the installation of a multidirectional inertia reel type safety harness, ensuring compliance with specified standards within a defined timeframe.
The Civil Aviation Safety Authority, as the enforcing body, schedules these airworthiness directives to maintain the highest safety standards in the Australian civil aviation sector. The directive for Airparts (NZ) Ltd. FU 24 Series Aeroplanes, specifically AD/FU24/41, requires operators of non-modified agricultural models to retrofit their aircraft with a suitable safety harness within six months of 30 September 1971. This measure is crucial in mitigating the risks associated with inadequate pilot restraint systems, thus safeguarding the lives of pilots and enhancing overall aviation safety.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to the aviation industry and is administered by the Civil Aviation Safety Authority (CASA). The scope of this particular legislation, AD/FU24/41, targets all models in the agricultural category of FU 24 Series Aeroplanes that have not been modified in accordance with the provisions of Supplemental Type Certificate 61-1, or an equivalent approved scheme that allows the use of a fixed type safety harness. This directive mandates that these aircraft must be modified to fit a multidirectional type inertia reel that complies with Specification IL-R-8236 Type MA2-MA4 or -MA6, or an alternative specification that is acceptable to the Secretary of CASA. The requirement necessitates that these modifications be completed within six months from 30 September 1971 to ensure compliance with safety standards. The regulations apply nationally across Australia and are not limited to any specific states or territories. There are no stated exclusions or exemptions mentioned within the scope of this directive, and it extends its application to all relevant aircraft within the specified category and conditions. Subordinate instruments may provide further details or modifications to the application of this directive as necessary.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39 - 105, contain specific Airworthiness Directives for various aircraft. One such directive is AD/FU24/41, which pertains to the installation of pilot restraints in the FU 24 Series Aeroplanes manufactured by Airparts (NZ) Ltd. This directive applies to all models in the agricultural category that have not been modified according to the Supplemental Type Certificate 61-1 or an equivalent approved scheme that allows for the use of a fixed type safety harness (section 9/71).
The main requirement of AD/FU24/41 is that the safety harness installation must be modified by fitting a multidirectional type inertia reel. This reel must comply with Specification IL-R-8236 Type MA2-MA4 or -MA6, or an alternative specification that is acceptable to the Secretary (section 9/71). This specification ensures that the inertia reel meets the necessary safety standards for the aircraft. The compliance with this directive must be achieved within six months from 30 September 1971.
The obligations imposed by this directive on the parties governed by it are primarily focused on ensuring that the safety harness installation is modified to meet the specified requirements. This involves the installation of an appropriate multidirectional inertia reel to enhance the safety of pilots operating the FU 24 Series Aeroplanes. The directive mandates that these modifications must be completed within a specific timeframe, underscoring the importance of timely compliance with safety regulations.
Failure to comply with AD/FU24/41 could lead to serious consequences. While the specific penalties for breach are not detailed in the extract, under the Civil Aviation Act 1988, non-compliance with Airworthiness Directives can result in significant penalties. These may include substantial fines and potential criminal charges for individuals or corporations that fail to adhere to the requirements set out by the Civil Aviation Safety Authority. Such penalties serve to reinforce the importance of adhering to safety directives to ensure the continued safety of aviation operations.