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 200/17 Nacelle Wheel Well Fender Installation 7/77
Applicability: All model 200 with high flotation landing gear installations up to S/No BB-188. Requirement: Action in accordance with Beechcraft SI No 0897.
Compliance: 1. Inspect within 100 hours time in service after 31 July 1977 and thereafter at intervals not exceeding 100 hours time in service until modified.
2. Modify before achieving 500 hours time in service.
Overview
The Civil Aviation Regulations 1998, as amended, govern the airworthiness and operation of aircraft in Australia, with Part 39 specifically addressing airworthiness directives. One such directive, AD/BEECH 200/17, was enacted to address a safety issue concerning the installation of nacelle wheel well fenders on Beechcraft 200 (Super King Air) Series aeroplanes. This directive applies to all model 200 aircraft with high flotation landing gear installations up to serial number BB-188. The policy objective of this directive is to ensure the continued airworthiness and safety of these aircraft by mandating specific inspection and modification procedures. The directive requires an initial inspection within 100 hours of time in service after 31 July 1977, with subsequent inspections at intervals not exceeding 100 hours until modifications are made, and requires modifications to be completed before the aircraft reaches 500 hours of time in service. This was enacted by the Civil Aviation Safety Authority, reflecting a commitment to maintaining high safety standards within Australia's civil aviation sector.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all Beechcraft 200 (Super King Air) series aeroplanes that are equipped with high flotation landing gear installations, up to serial number BB-188. This regulation mandates the installation of nacelle wheel well fenders as per Beechcraft Service Instruction No. 0897 to ensure compliance with airworthiness standards. The regulation applies to all operators of these aircraft, requiring them to inspect the nacelle wheel well fenders within 100 hours of time in service following 31 July 1977 and subsequently at intervals not exceeding 100 hours until the modification is completed. Additionally, operators must modify the nacelle wheel well fenders before the aircraft accumulates 500 hours of time in service. This regulation is enforced by the Civil Aviation Safety Authority, which has the authority to issue directives and oversee compliance within the Commonwealth of Australia, ensuring the safety and airworthiness of the specified aircraft models.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, provide detailed requirements for the airworthiness of Beechcraft 200 (Super King Air) Series aeroplanes through AD/BEECH 200/17 (subsections 1 and 2). This legislation mandates the installation of nacelle wheel well fenders for all model 200 with high flotation landing gear installations up to serial number BB-188. The directive aligns with Beechcraft Service Instruction No 0897, which outlines the specific procedures for implementing these modifications (subsection 3).
The obligations under these regulations require aircraft operators to inspect the nacelle wheel well fenders within 100 hours of time in service following 31 July 1977 and subsequently, at intervals not exceeding 100 hours time in service until the modifications are made (subsection 4). Furthermore, operators must modify the nacelle wheel well fenders before the aircraft achieves 500 hours of time in service (subsection 5). These provisions ensure that the structural integrity and safety of the aircraft are maintained in accordance with the latest standards set forth by the Civil Aviation Safety Authority (CASA).
Failure to comply with these directives can result in significant legal and safety repercussions. Under the Civil Aviation Act 1988, non-compliance may lead to enforcement actions by CASA, including fines and other penalties. The exact penalties are not specified within the excerpt provided, but typically, the severity of the penalty can depend on the nature and extent of the non-compliance. For instance, failure to conduct the required inspections or to make the necessary modifications could lead to grounding of the aircraft, resulting in operational disruptions and financial losses for the operator. Additionally, severe non-compliance could potentially result in criminal charges, with penalties including substantial fines and imprisonment for individuals found responsible for breaches of the regulations.