AD/SM-260/1 - Engine Mount - Modification

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, serve to regulate civil aviation safety within Australia, ensuring compliance with international standards and addressing any identified safety gaps in the aviation industry. Specifically, Part 39 - 105 within the Civil Aviation Regulations 1998 focuses on the Civil Aviation Safety Authority's (CASA) schedule of airworthiness directives, which include mandatory modifications and safety improvements for various aircraft types. The legislative instrument F2006B07068 pertains to SIAI Marchetti 260 Series Aeroplanes, detailing a specific airworthiness directive (AD/SM-260/1) concerning the engine mount modification for certain serial numbers. The directive aims to rectify a safety issue by mandating compliance with the requirement document for affected aircraft, thereby enhancing aviation safety and aligning with CASA's overarching policy objective of maintaining high safety standards in civil aviation.

Scope and Application

The Civil Aviation Regulations 1998, as part of the Civil Aviation Safety Authority's (CASA) broader regulatory framework, specifically address the airworthiness of aircraft through various directives, including the SIAI Marchetti 260 Series Aeroplanes Airworthiness Directive AD/SM-260/1. This directive mandates modifications to the engine mount for certain F260 series aeroplanes, namely those with serial numbers 003, 101 to 125, and 2-29. The applicability of this directive is strictly confined to these specified aircraft models, ensuring that only those particular aeroplanes are subject to the outlined compliance requirements. CASA's authority extends throughout the Commonwealth of Australia, enforcing these regulations to maintain the highest safety standards in civil aviation. The directive does not explicitly state exclusions or exemptions, but compliance must be achieved as per the detailed requirements outlined in the associated regulatory documents.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39, Section 105, contain critical provisions concerning airworthiness directives for certain aircraft models. This particular legislative instrument, AD/SM-260/1, pertains to the SIAI Marchetti 260 Series Aeroplanes and mandates modifications to the engine mount (Section 5/70). The applicability of this directive is explicitly stated for F260 series aircraft with specific serial numbers: 003, 101 to 125, and 2-29. Compliance with these requirements is to be detailed in the requirement document, SIAI Marchetti SB No. 260B3. For the parties and entities governed by these regulations, the primary obligation is to ensure that the specified modifications are completed on the relevant aircraft to maintain their airworthiness. This involves adherence to the detailed technical requirements outlined in the requirement document. Operators and owners of the affected aircraft must ensure that the modifications are performed by authorised personnel and that all work is logged and certified as compliant with the Civil Aviation Safety Authority's standards. Failure to comply with the airworthiness directive can lead to serious consequences. Under Section 105 of the Civil Aviation Regulations 1998, non-compliance is considered a breach of the regulations. Such breaches can result in civil penalties, which may include substantial fines. Additionally, the continued operation of a non-compliant aircraft could be deemed unsafe, potentially leading to further regulatory action, including grounding of the aircraft. The seriousness of these consequences underscores the importance of strict adherence to the airworthiness directives outlined in the legislation.