AD/AC-100/5 - Tubular Structure - Corrosion Proofing

Overview

The Civil Aviation Regulations 1998, specifically within Part 39 - 105, include the Civil Aviation Safety Authority Schedule of Airworthiness Directives which address the maintenance and safety requirements for various aircraft models. One such directive, AD/AC-100/5, pertains to the S.L. Industries Commander 100 Series and Volair 10 Series Aeroplanes, focusing on corrosion proofing of the tubular structure for aircraft with serial numbers ranging from 012 to 085. This directive was enacted to ensure the structural integrity and safety of these specific aeroplane models, addressing the potential for corrosion that could compromise flight safety. The policy objective behind this regulation is to mandate immediate compliance to maintain airworthiness standards, ensuring the safety and reliability of these aircraft in operation. This legislative instrument was issued under the authority of the Commonwealth of Australia to uphold stringent safety protocols within the civil aviation sector.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, which includes detailed specifications for maintaining the airworthiness of certain aircraft. This legislation applies to all S/Nos. 012 to 085 of the Aero Commander Model 100 Series and Volair 10 Series aeroplanes, mandating compliance with AD/AC-100/5 concerning the corrosion proofing of the tubular structure. This directive ensures that these aircraft maintain their structural integrity and safety standards as specified by the Civil Aviation Safety Authority. The geographic reach of these regulations is nationwide, covering all Commonwealth airspace, ensuring a uniform standard of airworthiness across Australia. There are no stated exclusions, exemptions, or thresholds within the specific directive AD/AC-100/5, and compliance must be met forthwith as indicated in the document Aero Commander Model 100 SB 1004. The application of these regulations may be extended or further detailed through subordinate instruments issued by the Civil Aviation Safety Authority.

Key Provisions

The Civil Aviation Regulations 1998, specifically in Part 39 - 105, includes an Airworthiness Directive (AD) aimed at ensuring the safety of certain models of aircraft. AD/AC-100/5 pertains to the corrosion proofing of the tubular structure of S.L. Industries Commander 100 Series and Volair 10 Series aeroplanes. This directive applies to all aircraft models with serial numbers ranging from 012 to 085. The directive mandates that these aircraft must comply with the specifications outlined in the Aero Commander Model 100 Service Bulletin 1004 and that compliance must be achieved immediately (sections 39 - 105). Under this directive, the parties responsible for ensuring compliance, typically the aircraft owners or operators, must take immediate action to inspect and, if necessary, repair the tubular structure of their aircraft to prevent corrosion. This involves following the detailed procedures and specifications provided in the referenced service bulletin to ensure that the structural integrity of the aircraft is maintained. The compliance must be achieved forthwith, highlighting the urgency and importance of this safety measure (section 39 - 105). Failure to comply with this directive could result in serious safety risks, as corrosion in the tubular structure can lead to structural failure, potentially resulting in accidents. Although specific penalties are not detailed within the text provided, non-compliance with Civil Aviation Regulations generally can result in significant penalties. These could include substantial fines, enforcement actions by the Civil Aviation Safety Authority, and in severe cases, grounding of the aircraft until compliance is achieved. The gravity of the consequences underscores the importance of adhering to these safety directives (sections 39 - 105).