AD/BEECH 56/14 - Second Row Seats

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, establish a comprehensive regulatory framework governing all aspects of civil aviation within the country. The regulations were introduced to ensure the safety and efficiency of air travel by setting stringent standards and requirements for aircraft, personnel, and operations. One of the key components of these regulations is Part 39, which outlines specific airworthiness directives aimed at maintaining and enhancing aircraft safety. This legislative instrument, F2006B04044, focuses on the Beechcraft 56TC (Turbo Baron) Series Aeroplanes, mandating the inspection and modification of second row seats to address identified safety concerns. The objective of this directive is to ensure the integrity of the aircraft's seating structure, thereby mitigating potential risks during flight.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to the Beechcraft 56TC (Turbo Baron) series aeroplanes. The legislation mandates that all models of this aircraft series must comply with the Airworthiness Directive AD/BEECH 56/14, which pertains to the second row seats. The directive requires an inspection of the rear attachment rails of the second row seats to ensure they have stops at the forward ends. If these stops are absent, the rails must be modified by fitting stop assemblies P/N 414-180657-3 or an equivalent approved by the Secretary. This directive applies across the Commonwealth of Australia and must be adhered to by all relevant entities, including aircraft owners, operators, and maintenance providers. The regulation aims to enhance safety standards within the aviation industry by ensuring that specific design features are implemented to prevent potential hazards. The directive is non-negotiable and must be complied with by the specified date of 31 July 1973, ensuring a uniform application across the jurisdiction.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105 (Civil Aviation Safety Authority Schedule of Airworthiness Directives), address the safety requirements for certain aircraft models through detailed airworthiness directives. For the Beechcraft 56TC (Turbo Baron) Series Aeroplanes, the directive AD/BEECH 56/14 focuses on the second row seats and their rear attachment rails. This directive mandates the inspection of the rear attachment rails of the second row seats for the presence of stops at their forward ends (Section 1). If the inspection reveals that the rails do not have these stops, the directive requires the installation of stop assemblies P/N 414-180657-3 or an equivalent approved by the Secretary (Section 2). This modification must be completed before 31 July 1973. Under these regulations, the parties governed—including aircraft owners, operators, and maintenance providers—bear specific obligations to ensure compliance. They must conduct the necessary inspections of the second row seats' rear attachment rails and identify whether the required stops are present. If the stops are missing, they must fit the specified stop assemblies or an equivalent part approved by the Secretary of the Department of Infrastructure and Transport. Failure to comply with these directives could result in the aircraft being deemed unairworthy, which could lead to grounding of the aircraft and legal repercussions for the operator. The consequences of non-compliance with these airworthiness directives are significant. While the specific penalties are not detailed in the text, non-compliance could result in severe civil or criminal penalties under broader aviation safety laws. Such penalties may include fines, operational restrictions, and potential legal action against the parties responsible for the aircraft. The seriousness of these potential outcomes underscores the importance of adhering to the specified directives to maintain the safety and airworthiness of the Beechcraft 56TC (Turbo Baron) Series Aeroplanes.