COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Boeing 727 Series Aeroplanes
AD/B727/80
Amdt 1
Horizontal Stabilizer Centre Section Front Spar Junction Fittings - Inspection
2/78
Applicability: All models.
Document: 1. FAA AD 77-18-06 Amdt. 39-3048; or
2. Boeing SB No. 55-A69, Rev. 1. Compliance: As per requirement document No. 1.
Overview
The Civil Aviation Regulations 1998, as amended by F2006B02784, were enacted to ensure the safe operation of civil aircraft within Australian airspace. This legislative instrument, introduced by the Australian Government, aims to address specific safety concerns associated with the operation of Boeing 727 Series Aeroplanes. The Regulations, administered by the Civil Aviation Safety Authority (CASA), focus on mandating rigorous safety directives to mitigate risks inherent in aviation operations. The policy objective of these regulations is to ensure that all aircraft, including the Boeing 727 Series, meet stringent airworthiness standards to protect the public and enhance the safety of air travel. Compliance with these directives is critical for operators to maintain the airworthiness of their aircraft, thereby supporting the overarching goal of public safety in civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all Boeing 727 Series aeroplanes registered in Australia, imposing mandatory requirements concerning the inspection of horizontal stabilizer centre section front spar junction fittings. The scope of this regulation extends to all operators of Boeing 727 aircraft within Australian jurisdiction, ensuring that these aircraft meet specified safety standards to maintain airworthiness. The geographic reach of this regulation is national, applying uniformly across the Commonwealth of Australia, and it is enforced by the Civil Aviation Safety Authority. The regulation mandates compliance with either the FAA AD 77-18-06 Amendment 39-3048 or Boeing Service Bulletin No. 55-A69, Revision 1, with no exclusions or exemptions provided, underscoring the importance of rigorous inspection protocols to ensure flight safety. The application of this regulation may also be extended or modified through subordinate instruments, aligning with broader aviation safety standards and technological advancements.
Key Provisions
The Civil Aviation Regulations 1998 (Cth), particularly Part 39 - 105, addresses the maintenance and airworthiness of aircraft, including specific requirements for Boeing 727 Series aeroplanes. Section 39 - 105 pertains to Airworthiness Directives (ADs) and specifies that all models of Boeing 727 aeroplanes must comply with certain maintenance procedures. Specifically, the amendment AD/B727/80 Amdt 1 mandates that the horizontal stabilizer centre section front spar junction fittings must be inspected as outlined in either the Federal Aviation Administration's AD 77-18-06 Amendment 39-3048 or Boeing Service Bulletin No. 55-A69, Revision 1. These directives aim to ensure the structural integrity of the aeroplane and maintain its airworthiness.
The obligations imposed by the Civil Aviation Regulations 1998 (Cth) on the operators and maintainers of Boeing 727 aeroplanes are stringent. Operators and maintainers must adhere to the inspection and maintenance requirements stipulated in the referenced FAA AD or Boeing SB. This includes conducting a thorough inspection of the horizontal stabilizer centre section front spar junction fittings to identify any potential defects, damage, or wear that could compromise the aeroplane's structural integrity. Compliance with these directives is mandatory, and failure to do so could result in severe consequences for air safety and regulatory compliance.
Failure to comply with the airworthiness directives outlined in the Civil Aviation Regulations 1998 (Cth) can lead to significant legal and operational repercussions. Non-compliance with AD/B727/80 Amdt 1 could result in the grounding of the aeroplane until the required inspections and repairs are completed. Furthermore, there are potential criminal and civil penalties for operators or maintainers who neglect to follow these directives. Under section 96 of the Civil Aviation Act 1988 (Cth), individuals or entities found in breach of airworthiness requirements may face fines of up to $210,000 for individuals and $1,050,000 for corporations, in addition to other civil liabilities. These stringent penalties underscore the importance of adhering to the specified maintenance procedures to ensure the safety and airworthiness of Boeing 727 aeroplanes.