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 200/1 Strobe Light Bonding Straps 1/75
Applicability: All model 200 with S/Nos BB-1 thru BB-14, BB-16 thru BB-21,and BB-29 fitted with Grimes P/N 30-0467-1 or Grimes P/N 30-0467-3 Strobe Light Assemblies.
Document: Action in accordance with Beechcraft SI No 0655-362, Rev 1. Compliance: Within 100 hours time in service after 31 January 1975.
Overview
The Civil Aviation Regulations 1998 were enacted to ensure the safety of civil aviation in Australia. Part 39 of these Regulations, which includes the Airworthiness Directives, was introduced to address the need for maintaining the airworthiness of aircraft and to ensure compliance with international standards and best practices. The policy objective is to maintain and enhance the safety of civil aviation through rigorous oversight and enforcement of airworthiness standards. In this context, the Civil Aviation Safety Authority (CASA) issues specific directives to address identified safety concerns, such as the requirement for strobe light bonding straps in Beechcraft 200 (Super King Air) Series Aeroplanes. These directives mandate compliance to mitigate risks and ensure aircraft remain airworthy, thereby protecting the public and maintaining the integrity of the aviation industry.
Scope and Application
The Civil Aviation Regulations 1998, as amended, under the Civil Aviation Act 1988, govern the safety and operation of aircraft within Australia's airspace. Specifically, Part 39 - 105 of these regulations details the authority's Schedule of Airworthiness Directives, which includes stringent safety requirements for various aircraft types. One such directive, AD/BEECH 200/1, pertains to the Beechcraft 200 (Super King Air) Series aeroplanes, addressing the bonding straps of strobe light assemblies. This directive applies to aircraft with serial numbers BB-1 through BB-14, BB-16 through BB-21, and BB-29 that are equipped with Grimes part numbers 30-0467-1 or 30-0467-3 strobe light assemblies. Compliance with this directive is mandatory within 100 hours of time in service following 31 January 1975, ensuring that the specified aircraft meet the required safety standards set by the Civil Aviation Safety Authority. The directive is enforceable across the entire Commonwealth of Australia, affecting both private and commercial operators of the affected aircraft models.
Key Provisions
The Civil Aviation Regulations 1998, particularly Part 39 - 105, establish the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which apply to specific aircraft models and configurations. One such directive, AD/BEECH 200/1, pertains to the Beechcraft 200 (Super King Air) Series Aeroplanes, specifically those with serial numbers BB-1 through BB-14, BB-16 through BB-21, and BB-29 that are equipped with Grimes P/N 30-0467-1 or Grimes P/N 30-0467-3 Strobe Light Assemblies (Section 1/75). The directive mandates compliance with Beechcraft Service Information (SI) No 0655-362, Revision 1. The requirement is for compliance to be achieved within 100 hours of time in service after 31 January 1975.
For the entities and parties governed by these regulations, the obligations are clear and direct. Owners and operators of the specified Beechcraft 200 (Super King Air) Series Aeroplanes must ensure that the Strobe Light Bonding Straps are installed and maintained in accordance with the specified Service Information. This involves a thorough inspection and, if necessary, the installation or repair of the bonding straps to meet the regulatory standards. Compliance must be documented and verified by CASA-approved personnel to ensure adherence to the directive.
The legislation also delineates the consequences of non-compliance with the airworthiness directive. Failure to comply with AD/BEECH 200/1 within the stipulated timeframe can result in serious ramifications. The primary consequence is the potential grounding of the affected aircraft until the required modifications are completed. In addition, operators may face civil penalties, which can include fines and other administrative actions as prescribed by the Civil Aviation Regulations. Additionally, non-compliance may lead to criminal charges, particularly if the failure to adhere to the directive results in a safety hazard or incident. The maximum penalties for such offences can be substantial, reflecting the critical nature of maintaining airworthiness standards.