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-N22/30 Horizontal Stabiliser Control System - Inspection for Wind Gust Damage
Applicability: All models N22 and N24.
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Requirement: 1. Inspect the horizontal stabiliser control stops and stop support structure for damage which may have been caused by wind gusts.
2. If damage is found proceed with the inspection requirements of GAF Alert SB No. ANMD-27-12.
Compliance: Unless already accomplished, before further flight.
Background: Wind gusts have caused damage to the lower fork end fitting of the stabiliser operating rod on several aeroplanes.
Overview
The Civil Aviation Regulations 1998, under the authority of the Australian Parliament, established a framework to ensure the safety of civil aviation in Australia. One of the critical components of these regulations is Part 39, which includes the Airworthiness Directives (AD) aimed at addressing specific safety concerns in aircraft operations. AD/GAF-N22/30 is an example of such directives, specifically targeting the GAF N22 and N24 series aeroplanes. This directive was introduced to address the problem of wind gust-induced damage to the horizontal stabiliser control system, particularly the lower fork end fitting of the stabiliser operating rod, which has caused issues in previous incidents. The policy objective is to enhance flight safety by mandating inspections and repairs to prevent potential failures due to such damage, ensuring compliance before further flight.
The Civil Aviation Safety Authority (CASA) issued AD/GAF-N22/30 to mandate that all N22 and N24 series aeroplanes undergo inspections of their horizontal stabiliser control stops and support structure for any wind gust-induced damage. If damage is detected, the directive requires adherence to the inspection procedures outlined in GAF Alert SB No. ANMD-27-12. This directive aims to mitigate the risk of in-flight incidents by ensuring that any identified damage is addressed promptly, thus maintaining the airworthiness of the aircraft and safeguarding the safety of all those on board.
Scope and Application
The Civil Aviation Regulations 1998, specifically PART 39 - 105, apply to all N22 and N24 series aeroplanes operated within the Commonwealth of Australia. This legislation mandates that all such aircraft must undergo a thorough inspection of their horizontal stabiliser control stops and support structure to detect any potential damage caused by wind gusts. This directive applies to all operators and owners of N22 and N24 series aeroplanes, ensuring that any damage identified must be addressed according to the inspection requirements outlined in GAF Alert SB No. ANMD-27-12 before any further flight can be undertaken. The regulations are enforced by the Civil Aviation Safety Authority (CASA) and are designed to maintain the safety standards of civil aviation within the country. The scope of these regulations is comprehensive, ensuring that all relevant entities comply with the stipulated safety measures to prevent accidents due to wind gust damage. The regulations do not specify any exclusions or exemptions but mandate strict compliance to maintain airworthiness and safety.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39, include a detailed directive for the airworthiness of GAF N22 and N24 series aeroplanes. In this context, the relevant sections are AD/GAF-N22/30, which focuses on the horizontal stabiliser control system. According to this directive (AD/GAF-N22/30), the primary requirement is to inspect the horizontal stabiliser control stops and the stop support structure for any damage potentially caused by wind gusts (Section 1). This inspection is crucial to ensure that no wind-induced damage has compromised the structural integrity of these components.
Compliance with AD/GAF-N22/30 mandates that the inspection be conducted before any further flight, unless it has already been completed (Section 2). This directive applies to all models of N22 and N24 aeroplanes. The background information provided in the directive highlights the issue of wind gusts causing damage to the lower fork end fitting of the stabiliser operating rod, which has been observed in several aeroplanes. This directive is a preventative measure to mitigate the risk of such damage leading to operational hazards.
Entities governed by the Civil Aviation Regulations 1998, particularly those operating GAF N22 and N24 series aeroplanes, must adhere to the requirements of AD/GAF-N22/30. This involves conducting thorough inspections of the horizontal stabiliser control stops and the stop support structure to identify any wind-induced damage. Operators must ensure that these inspections are performed before the aeroplane takes to the skies again if they have not already been carried out. This obligation underscores the importance of maintaining the structural integrity of critical components to ensure flight safety.
Failure to comply with the inspection requirements stipulated in AD/GAF-N22/30 may result in severe consequences. While the specific penalties are not detailed within the text of this directive, non-compliance with Civil Aviation Regulations 1998 generally can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions may include fines, operational restrictions, or even the grounding of the affected aeroplane until the necessary inspections are performed and any identified issues are resolved. The potential for such penalties underscores the importance of adhering strictly to the regulatory requirements to ensure the safety and airworthiness of the aircraft.