AD/BEECH 60/6 - Fin Spar

Overview

The Civil Aviation Regulations 1998, specifically within Part 39 - 105, address the maintenance and safety requirements for various aircraft, including the Beechcraft 60 (Duke) Series Aeroplanes. Enacted by the Parliament of the Commonwealth of Australia, this legislation aims to ensure that all aircraft operating within Australia comply with stringent safety standards to protect passengers and crew. This particular directive, AD/BEECH 60/6, targets the fin spar of specific models of the Beechcraft 60 (Duke) Series Aeroplanes, mandating compliance with Beechcraft Service Instruction No. 0336-134 within 100 hours of time in service after 29 May 1970. The overarching policy objective is to mitigate risks associated with structural integrity, thereby enhancing the overall safety of civil aviation in Australia.

Scope and Application

The Civil Aviation Regulations 1998, as amended, applies to specific Beechcraft 60 (Duke) Series aeroplanes, specifically those with serial numbers P-1 to P-117, P-120, P-124, and P-125. The regulation is issued under the authority of the Civil Aviation Safety Authority (CASA) and falls within the Commonwealth of Australia’s jurisdiction, meaning it has a national reach. The regulation mandates compliance with Beechcraft Service Instruction No. 0336-134 concerning the fin spar, which must be addressed within 100 hours of time in service after 29 May 1970. The regulation is designed to ensure the airworthiness of the specified aircraft by requiring specific maintenance actions to be taken within a defined timeframe. No exclusions, exemptions, or thresholds are mentioned in the text, and the application of the regulation is not extended or restricted by subordinate instruments.

Key Provisions

The key operative sections of the Civil Aviation Regulations 1998, specifically under Part 39 - 105, and the Schedule of Airworthiness Directives, focus on ensuring the safety and compliance of the Beechcraft 60 (Duke) Series Aeroplanes. Section AD/BEECH 60/6 pertains to the fin spar of the model 60 with serial numbers P-1 to P-117, P-120, P-124, and P-125. The directive mandates compliance with Beechcraft Service Instruction No. 0336-134 and requires action to be taken within 100 hours of time in service after 29 May 1970. The obligations and requirements imposed by the Act on the parties or entities it governs are clear and specific. Owners and operators of the affected Beechcraft 60 aeroplanes must adhere to the specified action outlined in Beechcraft SI No. 0336-134, which likely includes inspections, repairs, or replacements of the fin spar. These directives are designed to maintain the airworthiness and structural integrity of the aircraft, ensuring safety for passengers and crew. Failure to comply with the airworthiness directives set out in the regulations can result in serious consequences. While the specific civil and criminal penalties are not detailed in the excerpt, generally, under the Civil Aviation Act 1988, breaches of airworthiness directives can lead to significant fines and potential criminal charges. For instance, failing to comply with an airworthiness directive can result in substantial financial penalties, and in severe cases, criminal charges may be brought against the responsible party, leading to imprisonment. The exact penalties depend on the severity of the breach and the impact on aviation safety. It is imperative for aircraft owners, operators, and maintenance personnel to be fully aware of and comply with these directives to avoid any legal repercussions. Ensuring adherence to the specified requirements within the stipulated timeframe is crucial for maintaining the safety standards mandated by the Civil Aviation Regulations. The consequences of non-compliance not only risk the safety of the aircraft but also the potential for legal and financial penalties.