COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
SIAI Marchetti 260 Series Aeroplanes
AD/SM-260/3 Pilot Seat Stroke Limit Stops - Installation 12/71
Applicability: All F260 series with S/Nos. 101 to 125, 2-26 to 2-32, 2-34 to 2-41, 2-43 to 2-46, 2-49,
2-52 and 502.
Document: SIAI Marchetti SB No. 260B6.
Compliance: Within 100 hours time in service after 29 January 1972, or 2 months, whichever occurs first.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, form the backbone of the regulatory framework governing aviation safety in the country. These regulations aim to ensure that all civil aviation operations are conducted safely and efficiently. One specific legislative instrument under these regulations, F2006B07080, pertains to the installation of pilot seat stroke limit stops on SIAI Marchetti 260 Series aeroplanes. This legislative instrument was introduced to address safety concerns related to the operation of these specific aircraft models. The objective is to mitigate risks by ensuring that the pilot seat strokes do not exceed safe limits, thus enhancing overall flight safety. The regulation specifies the applicability to certain serial numbers of the SIAI Marchetti 260 Series aeroplanes and mandates compliance within a defined timeframe after a particular date. This ensures that all affected aircraft are modified to meet the prescribed safety standards, thereby reducing the likelihood of accidents related to pilot seat mechanisms.
Scope and Application
The Civil Aviation Regulations 1998, as amended, establish stringent safety standards across Australia's civil aviation industry, with the regulations encompassing a broad spectrum of aircraft types and operational aspects. Under PART 39 - 105, the specific Airworthiness Directive AD/SM-260/3 pertains to the installation of pilot seat stroke limit stops on SIAI Marchetti 260 Series aeroplanes. This directive applies to all F260 series aircraft with serial numbers ranging from 101 to 125, 2-26 to 2-32, 2-34 to 2-41, 2-43 to 2-46, 2-49, 2-52, and 502. The directive mandates compliance within 100 hours of time in service following 29 January 1972, or within two months, whichever occurs first, as referenced in SIAI Marchetti Service Bulletin No. 260B6. This regulation applies to all entities operating these specified aircraft within Australian airspace, ensuring adherence to critical safety measures. The scope of this legislation extends nationally, with enforcement falling under the jurisdiction of the Civil Aviation Safety Authority (CASA), and does not include any stated exclusions or exemptions. Subordinate instruments may further detail implementation and compliance requirements, thereby extending or clarifying the application of this directive.
Key Provisions
The main operative sections of the Civil Aviation Regulations 1998, specifically within PART 39 - 105, focus on the installation of pilot seat stroke limit stops on SIAI Marchetti 260 Series aeroplanes. The Airworthiness Directive (AD) AD/SM-260/3 mandates the installation of these limit stops on all F260 series aeroplanes with specific serial numbers, which include ranges from 101 to 125, 2-26 to 2-32, 2-34 to 2-41, 2-43 to 2-46, 2-49, 2-52, and 502. The directive references the SIAI Marchetti SB No. 260B6 document for compliance guidelines. The compliance period is set within 100 hours of time in service after 29 January 1972, or within 2 months, whichever occurs first.
The obligations and requirements imposed by these regulations on the parties governed are stringent. Aircraft operators must ensure that the specified models of the SIAI Marchetti 260 Series are inspected and, if necessary, have the pilot seat stroke limit stops installed according to the guidelines provided in the referenced document. This is to ensure the continued airworthiness and safety of the aircraft in operation. Compliance with the installation deadline is critical, as failure to adhere to the stipulated timeframe could result in the aircraft being deemed non-airworthy.
The Civil Aviation Regulations 1998 also outline the potential consequences for non-compliance with the AD. Any breach of the installation requirements can lead to severe civil and potentially criminal penalties. Specifically, failure to comply with an Airworthiness Directive can result in substantial fines and, in serious cases, criminal charges against the operators or individuals responsible for the oversight. While the exact maximum penalties are not detailed within the text, it is understood that non-compliance with such critical safety directives can attract significant legal repercussions. The overarching aim is to enforce strict adherence to safety standards to prevent accidents and ensure the safety of all persons onboard and on the ground.