COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
GAF N22 and N24 Series Aeroplanes
AD/GAF-N22/47 Engine Air Intake Modification 9/82
Applicability: All Nomad N22 and N24 series aeroplanes. Document: GAF SB No. NMD-71-6 Rev. 2.
Compliance: Before 30 June 1983.
Background: This modification is required to provide engine inlet icing protection over the full certification envelope.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, provide comprehensive rules governing civil aviation safety and operations within Australia. One specific aspect of these regulations is the management of Airworthiness Directives (ADs) through the Civil Aviation Safety Authority (CASA). One such AD, AD/GAF-N22/47, pertains to the GAF N22 and N24 series aeroplanes and mandates an engine air intake modification to protect against engine inlet icing. This AD was introduced to address the problem of engine inlet icing, which can compromise flight safety by potentially leading to engine failure during critical phases of flight. The policy objective behind this AD is to ensure that all applicable aircraft are compliant with the necessary safety modifications to prevent such hazards, thereby maintaining high standards of airworthiness and flight safety across the Australian civil aviation sector.
The regulation applies to all Nomad N22 and N24 series aeroplanes and requires compliance with the specified modifications before 30 June 1983. This directive is intended to safeguard the operational integrity and safety of these aircraft by providing comprehensive protection against the risks associated with engine inlet icing, aligning with the overarching goal of ensuring the highest safety standards in civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39, pertain to the airworthiness of aircraft and include a range of directives to ensure safety and compliance across the aviation industry. Among these, AD/GAF-N22/47 addresses the requirement for engine air intake modification for all Nomad N22 and N24 series aeroplanes to provide protection against engine inlet icing. This directive applies universally to all operators and owners of these specific aircraft models, ensuring that they meet the necessary safety standards set by the Civil Aviation Safety Authority (CASA). The directive mandates compliance before 30 June 1983, as outlined in GAF Service Bulletin No. NMD-71-6 Rev. 2. This regulation extends throughout the Commonwealth of Australia, impacting both domestic and international flights that involve these aircraft. The application of the directive is straightforward, without specific exclusions or thresholds mentioned, and it is enforced through subordinate instruments as specified within the broader regulatory framework of the Civil Aviation Regulations 1998.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, include a schedule of airworthiness directives that govern the maintenance and operation of various aircraft types. For the GAF N22 and N24 series aeroplanes, the relevant directive is AD/GAF-N22/47, which mandates an engine air intake modification to prevent engine inlet icing (AD/GAF-N22/47, 9/82). This directive applies to all aircraft in the specified series and must be implemented as outlined in GAF Service Bulletin No. NMD-71-6, Revision 2 (AD/GAF-N22/47). Compliance with this directive is required before 30 June 1983. The modification is intended to ensure that the aeroplanes maintain their airworthiness certification by providing necessary protection against engine inlet icing, which can compromise safety and performance.
The obligations imposed by this directive on the operators and owners of GAF N22 and N24 series aeroplanes are clear and specific. They must ensure that the engine air intake modification is carried out according to the detailed instructions provided in GAF Service Bulletin No. NMD-71-6, Revision 2. This involves inspecting the engine air intake system, replacing or modifying components as necessary, and ensuring that all modifications are properly documented. Operators must verify that the modifications have been completed before the specified compliance date of 30 June 1983 to maintain the airworthiness of their aircraft.
Failure to comply with the requirements set forth in AD/GAF-N22/47 can lead to serious consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce these regulations. If an operator fails to implement the required engine air intake modification, CASA may take action, including the potential grounding of the aircraft until the directive is complied with. Additionally, non-compliance can result in administrative penalties, including fines and other sanctions. The exact penalties can vary depending on the specific circumstances of the breach, but they are intended to ensure that safety standards are upheld and that aircraft remain airworthy.