COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Douglas DC4 Series Aeroplanes
AD/DC4/22 | Bus Bar Protector Plate - Installation | NK |
Document: | 1. Douglas SB (DC4) No. 90, dated 29 March 1948; or | |
| 2. ANO 105.1.16.2.5.21, Issue 2. | |
Overview
The Civil Aviation Regulations 1998, amended through legislative instrument F2006B08828, represent a critical piece of Australian legislation aimed at ensuring the safety and reliability of civil aviation operations. This regulation, overseen by the Civil Aviation Safety Authority, was enacted to address specific safety concerns associated with the Douglas DC4 series aeroplanes, particularly focusing on the installation of a bus bar protector plate. This directive was introduced to mitigate risks related to electrical faults that could compromise the aircraft's safety and operational integrity. The overarching policy objective of this regulation is to enforce mandatory safety standards that protect both the aircraft and its passengers, thereby maintaining the highest levels of safety in the national airspace. By issuing specific airworthiness directives, the Civil Aviation Safety Authority ensures compliance with these critical safety measures, thereby enhancing the overall safety framework of Australia’s civil aviation sector.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, pertains to the Airworthiness Directives for Douglas DC4 Series aeroplanes, focusing on the installation of a Bus Bar Protector Plate, as outlined in AD/DC4/22. This legislation applies to all persons and entities that own, operate, or maintain Douglas DC4 Series aeroplanes within the jurisdiction of the Commonwealth of Australia. The directive mandates compliance with the installation of the specified bus bar protector plate to ensure the airworthiness of the aircraft, thereby enhancing safety standards. The regulatory reach is confined to Australia's national airspace and is enforced by the Civil Aviation Safety Authority (CASA). There are no explicit exclusions or exemptions mentioned in the directive, meaning all Douglas DC4 Series aeroplanes must comply unless otherwise specified by subsequent or subordinate legislation. The application and enforcement of this directive may be extended or restricted through subordinate instruments issued by CASA, ensuring ongoing safety standards are met.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39, includes detailed provisions governing the airworthiness of aircraft, with section 39-105 focusing on the Douglas DC4 Series Aeroplanes. Section 39-105 mandates the installation of a bus bar protector plate on these aircraft (subsection 39-105(1)). This requirement is tied to the directives set out in the Airworthiness Directive AD/DC4/22, which references Douglas SB (DC4) No. 90 dated 29 March 1948, or ANO 105.1.16.2.5.21, Issue 2. The directive aims to ensure that the electrical system of the aircraft is adequately protected to prevent potential hazards such as short circuits or electrical fires.
Operators of Douglas DC4 Series Aeroplanes must comply with these provisions by installing the bus bar protector plate as specified. This involves ensuring that the installation adheres to the technical specifications and standards outlined in the referenced documents (subsection 39-105(2)). Operators must also maintain records of the installation and any subsequent inspections to demonstrate compliance with the regulations. This obligation extends to ensuring that the aircraft remains airworthy and that all components, particularly those related to the electrical system, are in a safe and operational condition.
Failure to comply with the requirements of section 39-105 can result in serious consequences. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement actions against operators who do not adhere to the Airworthiness Directives (subsection 39-105(3)). Non-compliance can lead to the imposition of administrative penalties, including fines, as well as potential criminal charges if the failure to comply results in a breach of safety regulations that causes harm or endangers safety (subsection 39-105(4)). The maximum penalties for these offences can be substantial, reflecting the importance of adhering to airworthiness standards to maintain public safety in civil aviation.