Overview

The Civil Aviation Regulations 1998, specifically Part 39, were enacted to ensure the safety and regulation of civil aviation within Australia. This legislation was introduced to address safety concerns in the aviation sector by providing comprehensive guidelines and requirements for airworthiness and operations. The Civil Aviation Safety Authority, established under this Act, is responsible for implementing and enforcing these regulations. One such regulation, AD/GAF-N22/48, pertains to the inspection of flap and aileron control rod fork ends on GAF N22 and N24 series aeroplanes to prevent instances where these components have been found compromised by water ingress. The policy objective behind this directive is to ensure that these aircraft maintain their airworthiness and comply with safety standards, thereby protecting the safety of passengers and crew.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39, applies to the safety and airworthiness of aircraft operating within Australia. Within this framework, the Civil Aviation Safety Authority (CASA) has issued Airworthiness Directives (ADs) to ensure that aircraft maintain a certain standard of safety. AD/GAF-N22/48 targets the GAF N22 and N24 series aeroplanes, more precisely those with serial numbers listed in Service Bulletin NMD-27-24. This directive mandates an inspection of the flap and aileron control rod fork ends to ensure they are free from water ingress, as instances have been identified where these parts were found full of water, potentially compromising the aircraft's safety. Compliance with this directive is required within 100 hours of time in service after 30 September 1983. The AD applies to all models N22, N22B, N24, and N24A with specific serial numbers, ensuring that these aircraft maintain their airworthiness within the Australian jurisdiction. The regulation does not explicitly state any exclusions or exemptions, but compliance is expected across all applicable aircraft within the specified timeframe.

Key Provisions

The key operative section of this legislation, AD/GAF-N22/48, pertains to the requirement for inspecting the flap and aileron control rod fork ends on GAF N22 and N24 series aeroplanes. Specifically, section 1 outlines the applicability of the directive to all models N22, N22B, N24, and N24A with serial numbers listed in Service Bulletin NMD-27-24. The directive mandates that this inspection be conducted within 100 hours of time in service after 30th September 1983, as detailed in section 3. The document referenced for compliance is GAF Service Bulletin NMD-27-24, which provides further detail on the inspection requirements. The obligations imposed by this legislation are clear and direct. Operators of the specified aircraft models must ensure that the flap and aileron control rod fork ends are inspected according to the stipulations set out in the Civil Aviation Regulations 1998. This inspection is intended to address instances where the rod fork ends have been found to be full of water, as mentioned in section 4. The requirement is that this inspection be carried out by a qualified individual or entity in accordance with the guidelines provided in Service Bulletin NMD-27-24. Non-compliance with these provisions can result in significant consequences. Under the Civil Aviation Regulations 1998, failure to adhere to the mandated inspections can lead to civil or criminal penalties. The specific nature of these penalties can vary, but they may include fines or other civil sanctions for individuals or entities that fail to comply. In more severe cases, criminal charges may be pursued, particularly if the non-compliance results in safety hazards or incidents. The exact penalties, including potential maximum fines, are governed by broader civil aviation laws and can be substantial, reflecting the critical importance of adhering to these safety directives.