AD/AMD 20/14 - Aileron Control Linkage

Overview

The Civil Aviation Regulations 1998, as amended by the legislative instrument F2006B02352, address the need for maintaining airworthiness standards for specific aircraft models to ensure the safety and reliability of civil aviation operations. Enacted by the Australian Government, these regulations are instrumental in directing the Civil Aviation Safety Authority (CASA) to issue Airworthiness Directives (ADs) for various aircraft types, including the Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) series. The policy objective behind this legislation is to mandate timely and consistent maintenance actions to mitigate potential safety risks, ensuring that aircraft continue to meet required safety standards. This particular AD/AMD 20/14 focuses on the aileron control linkage for specified serial numbers of the Fan Jet Falcon series, requiring compliance within a specified timeframe to maintain the integrity of the aircraft's control systems.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all Falcon 20 and Mystere-Falcon 200 series aeroplanes with specific serial numbers, namely those within the range 1 to 342, 344, 345, and 346. This legislation mandates that these aircraft must comply with Airworthiness Directives (AD) and Airworthiness Maintenance Directives (AMD) issued by the Civil Aviation Safety Authority (CASA). The requirement pertains to the aileron control linkage, necessitating action in accordance with the Service Bulletin (SB) No. 570 (ATA No. 27-75). Compliance must be achieved within 100 hours of time in service after 31 January 1978. The legislation is a Commonwealth regulation, thus its reach extends across the entire nation, ensuring uniform safety standards and regulatory oversight for these aircraft within Australian airspace. The Act does not specify any exclusions or exemptions within the provided excerpt and is enforced through subordinate instruments which may detail further requirements or operational conditions.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, establishes the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives. Within this, AD/AMD 20/14 pertains to the aileron control linkage of Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) series aeroplanes. This directive applies to all models with serial numbers (S/Nos.) ranging from 1 to 342, 344, 345, and 346. The requirement outlined in this directive mandates compliance with the Action in accordance with AMD Service Bulletin (SB) No. 570 (ATA No. 27-75). The directive stipulates that this action must be taken within 100 hours of time in service after 31 January 1978. The obligations imposed by AD/AMD 20/14 on the relevant parties, such as aircraft owners, operators, and maintenance service providers, are clear and specific. They must ensure that the aileron control linkage of the affected Fan Jet Falcon aeroplanes is modified as per the requirements of AMD SB No. 570. This involves adhering to the detailed technical instructions provided in the service bulletin to rectify any potential issues with the aileron control linkage. Ensuring compliance within the stipulated timeframe of 100 hours of time in service is critical to maintaining the airworthiness of the aircraft. Failure to comply with AD/AMD 20/14 can result in significant civil and criminal consequences. The Civil Aviation Safety Authority has the authority to enforce compliance with airworthiness directives. Non-compliance can lead to the issuance of enforcement actions, including fines, suspension or revocation of airworthiness certificates, and other regulatory penalties. In more severe cases, criminal charges may be pursued against individuals or corporations responsible for the non-compliance, leading to imprisonment or substantial fines. The maximum penalties for breaches of these regulations can be severe, reflecting the importance of ensuring the safety and airworthiness of civil aircraft.