AD/BEA 206/3 - Chafing of Hydraulic Master Switch/Lamp

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, form a comprehensive set of rules governing civil aviation safety. One of the specific regulatory instruments under this legislation is the Airworthiness Directives (ADs), which aim to ensure that aircraft remain airworthy through the enforcement of specific maintenance and repair actions. AD/BEA 206/3, issued in 1966, addresses a particular issue with the Beagle B206 Series aeroplanes, namely the chafing of the hydraulic master switch/lamp. The problem this directive targets is the potential for hydraulic lines to become damaged due to friction, which could compromise the aircraft's safety. The policy objective of this directive is to mandate compliance within a specified timeframe to prevent any operational risks associated with this identified safety issue.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, applies to the maintenance and airworthiness of certain aeroplane models within the Australian jurisdiction. This regulation pertains to the Beagle B206 Series 1 and 2 aeroplanes, with specific serial numbers mentioned in the directive. The regulation is enforced by the Civil Aviation Safety Authority (CASA) and mandates that the identified aeroplanes must adhere to the action detailed in Beagle Tech. Leaflet No. B206/TL/1 dated 1 September 1966 concerning the chafing of the hydraulic master switch/lamp. The directive requires compliance within 100 hours of the aeroplane's time in service from 15 February 1967. The scope of this regulation is strictly limited to the specified models and serial numbers, ensuring that only the designated aircraft are subject to the outlined safety directives.

Key Provisions

The Civil Aviation Regulations 1998, specifically in PART 39 - 105, establish a schedule of airworthiness directives that govern the safety standards for various aircraft models. One such directive, AD/BEA 206/3, addresses the issue of hydraulic master switch/lamp chafing for Beagle B206 Series aeroplanes (section 105.010). This directive is crucial for maintaining the operational safety of these aircraft and ensuring compliance with safety standards set by the Civil Aviation Safety Authority. Under this directive, specific models of the Beagle B206 Series, including those with serial numbers B005, B007, B013, B019, B022, B023, B026, B206/027, /028, /029, /032, and /035, are required to adhere to the action outlined in Beagle Tech. Leaflet No. B206/TL/1 dated 1 September 1966 (section 105.012). The requirement is for compliance within 100 hours of time in service from 15 February 1967. This means that any person or entity operating these aeroplanes must ensure that the hydraulic master switch/lamp is checked and addressed according to the specified technical leaflet to avoid potential hazards. The obligations imposed by this directive include the timely identification and rectification of any chafing issues with the hydraulic master switch/lamp. Operators and owners of the affected aeroplanes must ensure that the necessary modifications or repairs are carried out by qualified personnel, as specified in the technical leaflet, within the stipulated timeframe. Failure to comply with these obligations can result in the aeroplane being deemed unairworthy, which could lead to grounding and significant operational disruptions. Failure to comply with the airworthiness directive AD/BEA 206/3 can result in serious consequences. Civil penalties may be imposed under section 105.020 of the Civil Aviation Regulations 1998, which includes fines up to $153,000 for individuals and $765,000 for corporations. Additionally, criminal penalties may apply, with maximum fines and imprisonment terms for breaches of safety regulations. It is essential for operators and owners to strictly adhere to the directive to avoid these penalties and ensure the safety and airworthiness of their aircraft.