COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Douglas DC3 Series Aeroplanes
AD/DC3/11 Tailplane Rib - Modification NK
Document: 1. Douglas SB (C47A) No. 5; or
2. ANOs Part 100 Appendix “A” Notice 7/9; or 3. ANO 105.1.16.1.5.11.
Overview
The Civil Aviation Regulations 1998, as amended and enforced by the Civil Aviation Safety Authority (CASA), is a comprehensive regulatory framework governing all aspects of civil aviation in Australia. Specifically, Part 39 - 105 of these regulations focuses on Airworthiness Directives, which are legal mandates aimed at ensuring the continued safety of aircraft in operation. One such directive, AD/DC3/11, pertains to the modification of tailplane ribs on Douglas DC3 Series aeroplanes, addressing structural integrity issues that could potentially compromise flight safety. The directive was enacted to rectify problems identified in the structural design of certain aircraft models, ensuring compliance with the overarching policy objective of maintaining the highest standards of airworthiness and passenger safety.
The enactment of these regulations and directives is a statutory responsibility of the Australian Parliament, with CASA as the enforcing body. The primary policy objective behind the Civil Aviation Regulations 1998 and its associated directives is to safeguard the public by establishing stringent safety standards for aircraft operations. By mandating specific modifications and regular inspections, the legislation aims to mitigate risks associated with aircraft maintenance and operations, thereby ensuring the continued safety and reliability of Australia's civil aviation fleet.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all persons, entities, and industries involved in the operation, maintenance, and modification of civil aircraft within Australia. The regulation mandates compliance with the Airworthiness Directives issued by the Civil Aviation Safety Authority (CASA), which includes specific directives such as AD/DC3/11 concerning the modification of tailplane ribs in Douglas DC3 series aeroplanes. This directive applies to aircraft identified as Douglas SB (C47A) and those referenced in ANOs Part 100 Appendix “A” Notice 7/9 and ANO 105.1.16.1.5.11. The regulation's jurisdictional reach is nationwide, ensuring uniform standards across all states and territories. The application of these directives may be extended or restricted through subordinate instruments issued by CASA, which may include additional specifications or exemptions based on specific circumstances.
Key Provisions
The Civil Aviation Regulations 1998 (Cth), specifically in Part 39 - 105 of the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, addresses the modifications required for the Douglas DC3 Series aeroplanes. Section AD/DC3/11 mandates that a modification be made to the tailplane rib of these aeroplanes. This requirement is detailed in one of three referenced documents: Douglas SB (C47A) No. 5, ANOs Part 100 Appendix "A" Notice 7/9, or ANO 105.1.16.1.5.11. Essentially, the directive aims to ensure that the structural integrity of the tailplane rib is improved or altered to meet current safety standards.
The parties or entities governed by this directive, primarily the owners and operators of Douglas DC3 Series aeroplanes, have specific obligations under this legislation. They must ensure that the required modification to the tailplane rib is completed in accordance with the specified documents. This involves either conducting the modification themselves or engaging a certified repair facility that can perform the work to the required standard. Failure to comply with these modifications can lead to serious safety issues and potential non-compliance with civil aviation safety regulations.
Failure to adhere to the requirements set forth in AD/DC3/11 can result in significant legal and financial consequences. Section 98 of the Civil Aviation Act 1988 (Cth) stipulates that non-compliance with airworthiness directives can be considered an offence. The consequences for such offences can include substantial fines. Specifically, under section 98, the maximum penalty for contravening an airworthiness directive is a fine of up to $500,000 for an individual, and for a corporation, the fine can reach up to $2.5 million. Additionally, continued operation of an aircraft that does not comply with the airworthiness directive can result in further penalties, including potential grounding of the aircraft and further enforcement actions by the Civil Aviation Safety Authority.