AD/BEECH 200/7 - Rudder Push Rod Assembly

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, contain provisions governing aviation safety across the nation. This legislative instrument specifically targets the maintenance and operational standards of aircraft to ensure public safety and operational integrity. One such regulation, AD/BEECH 200/7, pertains to the rudder push rod assembly of Beechcraft 200 (Super King Air) Series aeroplanes, specifically for models with serial numbers BB-2 to BB-58. The regulation requires compliance with Beechcraft Service Instruction No 0778-153 and references FAA AD 76-03-07, mandating that corrective action be taken within 100 hours of time in service after 31 May 1976. This regulation was introduced to address identified safety concerns related to the rudder push rod assembly in the specified aircraft models, ensuring that these aircraft meet the necessary safety standards for continued operation.

Scope and Application

The Civil Aviation Regulations 1998, under Part 39 - 105, specifically addresses the airworthiness directives for certain aircraft models, including the Beechcraft 200 (Super King Air) Series Aeroplanes. This legislation applies to all Beechcraft 200 models with serial numbers BB-2 to BB-58, mandating compliance with specific safety requirements concerning the rudder push rod assembly. The directive requires action in accordance with Beechcraft Service Information No 0778-153 and notes the relevance of FAA AD 76-03-07 for additional context. The regulation necessitates that the specified action be undertaken within 100 hours of time in service after the directive's effective date of 31 May 1976. The scope of this regulation is nationwide, applying across all jurisdictions within Australia, ensuring a consistent standard of safety and compliance across the civil aviation industry. This regulation does not exclude any particular entities or operations, and its application is mandatory for the specified aircraft models within the stipulated timeframe.

Key Provisions

The Civil Aviation Regulations 1998, specifically in Part 39 - 105, detail the requirements for airworthiness directives related to certain aircraft models. For instance, AD/BEECH 200/7 pertains to the Beechcraft 200 (Super King Air) Series Aeroplanes and mandates specific action regarding the rudder push rod assembly (section 5/76). This directive applies to all models with serial numbers ranging from BB-2 to BB-58. The requirement is that the action must be taken in accordance with Beechcraft Service Instruction No 0778-153, with reference to FAA AD 76-03-07. Compliance with this directive must be achieved within 100 hours of time in service after 31 May 1976. Entities and individuals governed by this regulation must ensure that the specified maintenance action on the rudder push rod assembly is performed within the stipulated timeframe. This involves following the procedures outlined in the referenced service instruction to maintain the airworthiness of the aircraft. Compliance with these directives is crucial to avoid any potential safety issues that could arise from the failure to address the specified maintenance requirements. Failure to adhere to the airworthiness directive AD/BEECH 200/7 can result in significant legal and safety consequences. The Civil Aviation Safety Authority (CASA) enforces these regulations strictly, and non-compliance can lead to penalties. These penalties may include fines and other civil or criminal actions as prescribed under the Civil Aviation Act 1988. The severity of the penalties depends on the nature and extent of the non-compliance but can be substantial, underscoring the importance of adhering to the directives to ensure the safety and airworthiness of the aircraft.