AD/BEA 206/1 - Rudder Mass Balance

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, provide a comprehensive framework for ensuring the safety of civil aviation operations within the country. Specifically, Part 39 - 105 of these regulations includes a schedule of airworthiness directives, one of which is AD/BEA 206/1, relating to the rudder mass balance of Beagle B206 Series Aeroplanes. This legislation was introduced to address the need for maintaining specific aircraft components to ensure their continued airworthiness and safety. The policy objective, as reflected in these regulations, is to mandate routine inspections and adherence to service bulletins issued by the manufacturer to prevent potential safety issues arising from component degradation or malfunction. The enactment of these regulations by the Parliament aims to uphold high safety standards in civil aviation, ensuring the protection of passengers, crew, and the general public.

Scope and Application

The Civil Aviation Regulations 1998, under Part 39 - 105, specifically addresses the safety requirements for civil aviation within Australia, applying to a range of entities and individuals involved in the operation of aircraft. For the Beagle B206 Series aeroplanes, the regulations mandate adherence to Airworthiness Directives such as AD/BEA 206/1 concerning the rudder mass balance. This directive applies to all aircraft within the specified model series and requires compliance through periodic inspections, as outlined in the Beagle Service Bulletin B206/1 dated 13 December 1965, to ensure that the rudder mass balance remains within acceptable parameters. The regulations impose an inspection interval of no more than 100 hours of service time until the specified modification (Beagle Mod. 440) is incorporated. These safety directives are enforceable across the Commonwealth, ensuring a standardised approach to aviation safety throughout Australia, with the Civil Aviation Safety Authority overseeing compliance.

Key Provisions

The Civil Aviation Regulations 1998, under PART 39, specify the requirements for airworthiness directives, including AD/BEA 206/1 concerning the rudder mass balance of Beagle B206 Series aeroplanes (Section 39.105). This directive mandates that the action specified in Beagle Service Bulletin B206/1 dated 13 December 1965 be implemented. Specifically, this involves inspecting the rudder mass balance at intervals not exceeding 100 hours of time in service until the modifications outlined in Beagle Model 440 are incorporated. The entities governed by these regulations, particularly aircraft operators and maintenance personnel, must ensure that the inspections and actions specified in the directive are meticulously followed. Operators of the Beagle B206 Series aeroplanes need to adhere strictly to the inspection intervals and any required modifications to maintain the aircraft's airworthiness. Maintenance personnel must be trained and certified to perform these inspections and any necessary modifications to the rudder mass balance, ensuring that all work is done in compliance with the specified standards and procedures. Failure to comply with the provisions outlined in AD/BEA 206/1 can result in serious legal and safety consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce these regulations, and non-compliance can lead to penalties, including fines and potential grounding of the aircraft. The specific penalties are not detailed in the provided text, but they can include substantial financial penalties under the Civil Aviation Act 1988, as well as potential criminal charges in cases of gross negligence or wilful disregard for safety regulations. It is imperative for all parties involved to take the requirements seriously to avoid these repercussions.