COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 60 (Duke) Series Aeroplanes
AD/BEECH 60/35 Elevator Control Push Rods 5/80
Applicability: All models 60, A60 and B60 with S/Nos. P-3 to P-487. Requirement: Action in accordance with Beechcraft SI No. 1019.
Compliance: Within 100 hours’ time in service after 31 May 1980.
Background: Corrosion has been found in the elevator pushrods of other Beechcraft models which have pushrods of similar manufacture.
Overview
The Civil Aviation Regulations 1998 were enacted by the Parliament of the Commonwealth of Australia to ensure safety and regulation in civil aviation. The regulations address various safety aspects, including airworthiness directives, which are critical in maintaining the safety and integrity of aircraft in operation. One such directive, AD/BEECH 60/35, pertains specifically to the elevator control push rods of Beechcraft 60 (Duke) Series Aeroplanes. This directive was introduced to address the identified problem of corrosion in the elevator pushrods, which has been found in other similarly manufactured models. The policy objective behind this directive is to ensure that all affected aircraft are inspected and maintained in accordance with specified requirements to prevent potential safety hazards. Compliance with the directive is mandatory for all models 60, A60, and B60 with serial numbers P-3 to P-487, requiring corrective action within 100 hours’ time in service after 31 May 1980, following the specified Beechcraft Service Instruction No. 1019.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, sets forth the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, governing the maintenance and operation of aircraft in Australia. The particular Airworthiness Directive AD/BEECH 60/35 pertains to Beechcraft 60 (Duke) series aeroplanes, including all models 60, A60, and B60, with serial numbers ranging from P-3 to P-487. This directive mandates compliance with Beechcraft Service Instruction No. 1019, which addresses issues of corrosion found in elevator control push rods in similar models. Compliance with this directive is required within 100 hours of time in service following 31 May 1980. The directive applies to specified aircraft models within the Commonwealth of Australia and ensures that identified safety issues are addressed to maintain airworthiness standards. This legislation directly affects aircraft operators and maintenance personnel responsible for the specified Beechcraft models, ensuring that they adhere to the mandated safety instructions and maintain the aircraft's airworthiness.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, detail the Civil Aviation Safety Authority's (CASA) schedule of airworthiness directives, focusing on the Beechcraft 60 (Duke) Series Aeroplanes. The directive AD/BEECH 60/35 pertains to the elevator control pushrods and is applicable to all models 60, A60, and B60 with serial numbers (S/Nos.) P-3 to P-487. This directive mandates that all affected aircraft must comply with Beechcraft Service Instruction (SI) No. 1019. The requirement is to take action within 100 hours of time in service after 31 May 1980, reflecting CASA's proactive approach to maintaining airworthiness by addressing potential corrosion issues in the elevator pushrods, which have been identified in other similarly manufactured models.
Under these regulations, the parties or entities governed by the AD/BEECH 60/35 directive, primarily the aircraft owners, operators, and maintenance providers, are obligated to ensure that the specified maintenance action is performed on the elevator control pushrods within the prescribed timeframe. This involves adhering to the detailed instructions outlined in Beechcraft SI No. 1019, which may include inspection, repair, or replacement of the pushrods as necessary to prevent corrosion and maintain the safety and airworthiness of the aircraft.
Failure to comply with the requirements of the AD/BEECH 60/35 directive can result in significant consequences. While the specific regulatory text does not detail the exact nature of the penalties or consequences, non-compliance with CASA directives generally can lead to enforcement actions under the Civil Aviation Act 1988. These may include fines, legal action, and potential grounding of the aircraft until compliance is achieved. The severity of the penalties reflects the importance of adhering to airworthiness directives to ensure the safety of passengers and crew, as well as the integrity of the aviation system.