COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Kitfox Series Aeroplanes
AD/KITFOX/2 Flaperon Mass Balance 5/90
Applicability: All models not fitted with mass balance system (WMB 40).
Requirement: Carry out installation of flaperons mass balance system (WMB 40) in accordance with wing construction section of Denney Aerocraft Company, Kitfox Assembly Manual, or other scheme approved by the Authority.
Compliance: Prior to 30 June 1990.
Background: Flutter has occurred in both overseas and local aircraft. The company has made standard the fitting of a flaperon mass balance system and provides a kit for retrofit to aircraft not so equipped.
Overview
The Civil Aviation Regulations 1998 were enacted to regulate aviation safety across Australia, providing a comprehensive framework for the operation of civil aircraft. Specifically, Part 39 - 105 of the Civil Aviation Regulations includes Airworthiness Directives that are issued by the Civil Aviation Safety Authority (CASA) to address safety issues as they arise. The directive AD/KITFOX/2 pertains to the Kitfox Series Aeroplanes and was introduced to address the problem of flutter in aircraft not fitted with a mass balance system. This legislative instrument aims to ensure the installation of a flaperon mass balance system, as specified in the Denney Aerocraft Company, Kitfox Assembly Manual or an approved alternative, for all affected models to mitigate safety risks.
The policy objective of this directive is to enhance the safety of civil aviation by preventing flutter in Kitfox Series Aeroplanes through the mandatory installation of a mass balance system. The directive was enacted by CASA under the authority granted by the Civil Aviation Act 1988, and it requires compliance by 30 June 1990. This measure was implemented following reported incidents of flutter in both overseas and local aircraft, prompting the need for a regulatory response to ensure the continued safety of these aircraft in operation.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 – 105, mandates the installation of a flaperon mass balance system (WMB 40) on Kitfox Series Aeroplanes that are not already fitted with such a system. This applies to all models of Kitfox aeroplanes that lack the specified mass balance system, necessitating compliance with the wing construction section of the Denney Aerocraft Company's Kitfox Assembly Manual or an alternative scheme approved by the Civil Aviation Safety Authority (CASA). The requirement for compliance with this Airworthiness Directive must be fulfilled prior to 30 June 1990. The directive is in response to documented instances of flutter in both overseas and Australian aircraft, prompting the manufacturer to standardise the installation of the flaperon mass balance system and provide a retrofit kit for non-compliant aircraft. The scope of the legislation encompasses all entities involved in the manufacture, maintenance, and operation of Kitfox Series Aeroplanes within the Commonwealth of Australia, ensuring that these aircraft meet the necessary safety standards to mitigate the risk of flutter.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates certain safety provisions through Airworthiness Directives (AD) for the Kitfox Series Aeroplanes. One such directive, AD/KITFOX/2, focuses on the flaperon mass balance for all models not fitted with the mass balance system (WMB 40) (section 5/90). This directive requires the installation of a flaperon mass balance system in compliance with the wing construction section of the Denney Aerocraft Company, Kitfox Assembly Manual, or an alternative scheme approved by the Civil Aviation Safety Authority (CASA) (section 5/90).
The obligations imposed by this directive necessitate that aircraft owners or operators ensure the installation of the specified mass balance system to mitigate the risk of flutter, which has been reported both overseas and locally (section 5/90). This installation must be completed in accordance with the guidelines provided in the Denney Aerocraft Company’s manual or an approved alternative, ensuring the safety and airworthiness of the aircraft. Compliance with this directive must be achieved prior to 30 June 1990, establishing a clear timeline for the necessary modifications (section 5/90).
Breach of the requirements outlined in this Airworthiness Directive may lead to significant consequences. While the specific penalties for non-compliance are not detailed in the provided text, non-compliance with CASA directives typically results in serious repercussions under the Civil Aviation Act 1988. Offences may include fines, imprisonment, or both, depending on the severity and impact of the breach on aviation safety. The potential penalties underscore the importance of adhering to CASA’s regulations to maintain the safety standards required in civil aviation.