AD/BEECH 35/55 - Ruddervator Control Push Rods

Overview

The Civil Aviation Regulations 1998, specifically in Part 39 - 105, address the safety requirements for various aircraft, including the Beechcraft 35 (Bonanza) Series Aeroplanes. Enacted by the Australian Parliament, this legislation aims to ensure that all aircraft meet certain safety standards to protect the public and maintain the integrity of the aviation industry. The regulation in question, AD/BEECH 35/55, targets a specific issue with the ruddervator control pushrods in certain models of the Beechcraft 35 series, which could potentially be misaligned or suffer from internal corrosion, thereby compromising the aircraft's safety. The policy objective is to mandate compliance with Beechcraft Service Information No. 0989 within a specified timeframe, ensuring that these safety concerns are addressed promptly. This legislative instrument underscores the importance of ongoing maintenance and safety checks to mitigate risks associated with aircraft operation. By specifying a compliance deadline of 100 hours of time in service after 30 June 1980, the regulations aim to prevent potential hazards that could arise from the identified issues with the ruddervator control pushrods, thus enhancing overall aviation safety.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority’s (CASA) Schedule of Airworthiness Directives, which applies to all Beechcraft 35 series aeroplanes. These include models 35, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC, V35B, and V35B-TC with serial numbers ranging from D-1 to D-10187. The legislation mandates compliance with the requirements set forth in Beechcraft Service Instruction No. 0989, which addresses the potential issues of misalignment and internal corrosion affecting the ruddervator control pushrods. This directive must be adhered to within 100 hours of the aeroplanes’ time in service after 30 June 1980. The scope of this regulation extends across the Commonwealth of Australia, ensuring safety standards are uniformly applied to the specified aircraft within this jurisdiction.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, specifically in PART 39 - 105 concerning the Civil Aviation Safety Authority Schedule of Airworthiness Directives for the Beechcraft 35 (Bonanza) Series Aeroplanes, include the requirement outlined in AD/BEECH 35/55 (section 6/80). This directive pertains to the ruddervator control push rods of certain models of the Beechcraft 35 series aeroplanes, specifically those with serial numbers D-1 to D-10187. The directive mandates that compliance must be achieved by following the instructions provided in Beechcraft Service Instruction No. 0989. The compliance timeframe is set at 100 hours of time in service after 30 June 1980. The obligations imposed by this legislation on the parties governed by it include ensuring that the specified Beechcraft 35 series aeroplanes have their ruddervator control push rods checked and, if necessary, aligned or replaced in accordance with the instructions outlined in Beechcraft SI No. 0989. This action must be undertaken within the specified 100 hours of time in service post 30 June 1980 to maintain the airworthiness of the aircraft. The directive is designed to mitigate the risk of misalignment and internal corrosion of the ruddervator control push rods, which could potentially affect the safe operation of the aircraft. Breaching the requirements set out in this directive can result in civil or criminal consequences. Under the Civil Aviation Act 1988, non-compliance with airworthiness directives can be considered an offence. The potential penalties for such breaches can include fines and, in severe cases, imprisonment. The exact penalties depend on the nature and severity of the breach, but the potential consequences underscore the importance of adhering to the regulations to ensure aviation safety. The maximum penalties for offences under the Civil Aviation Act 1988 can be substantial, reflecting the critical nature of maintaining airworthiness in civil aviation.