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 200/8 Seat Locking Pins 5/76
Applicability: All model 200 with S/Nos BB-6 to BB-87, BB-89 to BB-99 and BB-101 to BB-106; All model A200 with S/Nos BC-1 to BC-8 and BD-1 to BD-8.
Requirement: Action in accordance with Beechcraft SI No 0789-314.
Note: FAA AD 76-04-02 refers.
Compliance: Within 100 hours time in service after 31 May 1976.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serve as a comprehensive framework for ensuring the safety and efficiency of civil aviation within the country. A specific section within this extensive regulation is Part 39, which addresses the safety directives that must be adhered to by various aircraft types, including the Beechcraft 200 (Super King Air) Series Aeroplanes. This particular regulation was introduced to address the need for maintaining stringent safety standards in civil aviation, ensuring that all aircraft meet specific airworthiness criteria, particularly for older models that may require periodic safety upgrades or modifications.
The Civil Aviation Safety Authority (CASA) is the enforcing body responsible for the oversight and implementation of these regulations. The policy objective behind the introduction of this regulation is to maintain the highest possible safety standards in the aviation sector by issuing specific directives for various aircraft models, such as the Beechcraft 200 series. These directives include requirements for seat locking pins, as detailed in AD/BEECH 200/8, and mandate compliance within a specified timeframe, such as within 100 hours of time in service after a certain date, in this case, 31 May 1976.
Scope and Application
The Civil Aviation Safety Authority Schedule of Airworthiness Directives, as part of the Civil Aviation Regulations 1998, specifically addresses the maintenance and safety requirements for certain Beechcraft 200 (Super King Air) Series Aeroplanes, detailing the mandatory actions to be taken concerning seat locking pins for specified serial numbers. This regulation applies to all model 200 aeroplanes with serial numbers ranging from BB-6 to BB-87, BB-89 to BB-99, and BB-101 to BB-106, as well as all model A200 aeroplanes with serial numbers BC-1 to BC-8 and BD-1 to BD-8. The requirement mandates adherence to Beechcraft Service Instruction No 0789-314, with reference to FAA AD 76-04-02, and compliance must be achieved within 100 hours of time in service after 31 May 1976. This regulation ensures that the specified aircraft models meet the necessary safety standards set forth by the Civil Aviation Safety Authority, thereby safeguarding air travel for the operators and passengers of these aircraft.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes the Civil Aviation Safety Authority Schedule of Airworthiness Directives, which details the requirements for the Beechcraft 200 (Super King Air) series aeroplanes. Section AD/BEECH 200/8 pertains to seat locking pins, with applicability to certain serial numbers of model 200 and model A200 Beechcraft aeroplanes. The directive requires actions in accordance with Beechcraft Service Information No. 0789-314, with a reference to FAA AD 76-04-02. Compliance with these directives must be achieved within 100 hours of time in service after 31 May 1976.
The obligations imposed by these regulations are significant for the aircraft operators and maintenance personnel of the specified Beechcraft aeroplanes. They must ensure that the seat locking pins are addressed as per the instructions outlined in Beechcraft SI No 0789-314. This involves checking the condition of the seat locking pins and following the recommended actions to maintain the airworthiness of the aircraft. Compliance must be achieved within the specified timeframe to avoid any potential safety issues.
Failure to comply with these airworthiness directives can lead to serious consequences. Non-compliance with the Civil Aviation Regulations 1998 can result in the aircraft being deemed unairworthy, which may prevent it from operating. For individuals or entities, this can lead to substantial financial penalties, as well as potential legal action. The exact penalties and consequences are detailed in other sections of the Civil Aviation Act 1988 and the Civil Aviation Regulations 1998, but they can include fines and, in severe cases, imprisonment. The severity of the penalties reflects the importance of adhering to these airworthiness directives to ensure the safety of all those involved in aviation activities.