AD/GAF-N22/21 Amdt 1 - Control Wheel Assembly Retaining Pin - Inspection

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, are a comprehensive set of rules governing all aspects of civil aviation in Australia. These regulations were introduced to ensure the safety and efficiency of civil aviation operations, and they include provisions for aircraft airworthiness, licensing, operations, and maintenance. One specific legislative instrument within these regulations is the Civil Aviation Safety Authority Schedule of Airworthiness Directives, which outlines mandatory directives to address safety issues. For instance, AD/GAF-N22/21 Amendment 1 pertains to the inspection of the control wheel assembly retaining pin for GAF N22 and N24 series aeroplanes, as specified in GAF Alert SB AN22-27-8. The directive mandates compliance within 10 hours of time in service after 3 July 1978, aiming to enhance the safety of these aircraft by ensuring the integrity of critical components. This specific directive was issued to address identified safety concerns and ensure adherence to safety standards set forth by the Civil Aviation Safety Authority.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates the compliance of airworthiness directives issued by the Civil Aviation Safety Authority (CASA) concerning the GAF N22 and N24 Series Aeroplanes. This legislation applies to all operators of these aircraft types within the Commonwealth of Australia, ensuring that the specified maintenance and inspection requirements are adhered to for safety and regulatory compliance. The directive AD/GAF-N22/21 Amendment 1 pertains to the inspection of the Control Wheel Assembly Retaining Pin, as outlined in GAF Alert SB AN22-27-8, with compliance expected within 10 hours of time in service after the directive's effective date of 3 July 1978. This regulation does not specify exclusions or exemptions, thereby encompassing all relevant aircraft operators and ensuring a consistent standard of maintenance and safety across the industry. The authority of CASA extends to enforce these regulations through subordinate instruments, ensuring thorough implementation and adherence.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 and specifically the 105th Civil Aviation Safety Authority Schedule of Airworthiness Directives (AD/GAF-N22/21 Amendment 1), addresses the inspection of the Control Wheel Assembly Retaining Pin on GAF N22 and N24 series aeroplanes. According to section 39-105, the directive is applicable as detailed in GAF Alert SB AN22-27-8, with the relevant document being GAF Alert SB AN22-27-8 Revision 1. Compliance with this directive is required within 10 hours of time in service after 3 July 1978. The obligations under this directive include ensuring that all inspections of the Control Wheel Assembly Retaining Pin are carried out by qualified personnel in accordance with the specifications provided in GAF Alert SB AN22-27-8. This means that the aircraft operator must ensure that the inspection is performed meticulously to maintain the airworthiness of the aircraft, as detailed in the referenced GAF Alert. Compliance involves documenting the inspection and ensuring that any necessary repairs or replacements are made to meet the safety standards set out in the regulations. Failure to comply with the requirements of this Airworthiness Directive can lead to significant consequences. Section 92 of the Civil Aviation Act 1988 imposes penalties for non-compliance with airworthiness directives, which can include fines and imprisonment for individuals and corporations. The exact penalties depend on the severity of the breach and the discretion of the court. Additionally, continued operation of an aircraft that does not comply with an Airworthiness Directive may result in the aircraft being grounded, further impacting the operator's ability to conduct flights and potentially leading to civil liabilities for any resulting damages or injuries.