COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 200 (Super King Air) Series Aeroplanes
AD/BEECH 200/16 Rudder Control System 6/77
Applicability: All model with S/Nos BB-2 to BB-38. Requirement: Action in accordance with Beechcraft SI No 0882.
Compliance: Within 100 hours time in service after 30 June 1977.
Overview
The Civil Aviation Regulations 1998, under Part 39 - 105, include a legislative instrument concerning airworthiness directives for specific aircraft models, notably the Beechcraft 200 (Super King Air) Series Aeroplanes. This legislation was introduced to address safety concerns within the aviation industry by ensuring that certain models adhere to specific maintenance and operational standards. The Civil Aviation Safety Authority, as the enacting body, mandates compliance with these directives to uphold the highest safety standards for civil aviation. The policy objective is clearly stated as ensuring that all applicable aircraft are maintained to prevent potential safety issues, particularly focusing on the rudder control system for the specified serial numbers.
This legislative instrument, specifically AD/BEECH 200/16, targets Beechcraft 200 series aeroplanes with serial numbers BB-2 to BB-38, requiring compliance with Beechcraft Service Instruction No 0882. The requirement necessitates that action be taken within 100 hours of time in service after 30 June 1977. The overarching goal is to mitigate risks associated with the rudder control system, ensuring that these aircraft meet the necessary safety criteria before continuing operations.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, apply to the maintenance and airworthiness of the Beechcraft 200 (Super King Air) Series aeroplanes, with serial numbers BB-2 to BB-38. This regulation mandates that operators of these aircraft must adhere to the airworthiness directive AD/BEECH 200/16, which focuses on the rudder control system. Compliance with this directive is essential to ensure the safety of the aircraft, and it requires action in accordance with Beechcraft Service Instruction No 0882. The directive must be implemented within 100 hours of time in service after 30 June 1977. The regulations apply to all persons and entities operating these specific Beechcraft 200 aeroplanes within Australia and its territories, ensuring that the safety standards set by the Civil Aviation Safety Authority are met across the Commonwealth. The regulations do not specify any exclusions, exemptions, or thresholds beyond the serial numbers and timeframe mentioned, and any further application or interpretation of these regulations may be governed by subordinate instruments issued by the Civil Aviation Safety Authority.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes an Airworthiness Directive (AD) for Beechcraft 200 (Super King Air) Series Aeroplanes, focusing on the rudder control system (Section 39-105). The directive, AD/BEECH 200/16, applies to all models with serial numbers BB-2 to BB-38. The requirement is for action to be taken in accordance with Beechcraft Service Instruction (SI) No 0882. Compliance with these directives must be achieved within 100 hours of the aeroplanes being in service after 30 June 1977.
The AD imposes specific obligations on the operators of the affected aircraft. Operators must ensure that the rudder control system of their Beechcraft 200 (Super King Air) aeroplanes is examined and actioned in accordance with the detailed instructions outlined in Beechcraft SI No 0882. This includes adhering to the specific timeline for compliance, which is within 100 hours of the aeroplanes being in service after the date of the directive, 30 June 1977. These obligations are designed to maintain the safety and airworthiness of the aircraft in question.
Failure to comply with the requirements set out in the AD/BEECH 200/16 can result in significant consequences. Under the Civil Aviation Regulations 1998, non-compliance may lead to enforcement actions by the Civil Aviation Safety Authority (CASA). The potential penalties for breaching these directives can include fines and other civil or criminal sanctions, depending on the severity and frequency of the non-compliance. The maximum penalties for such breaches are outlined in the broader regulatory framework, which may include substantial fines and potential imprisonment for serious or repeated violations.