COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Boeing 727 Series Aeroplanes
AD/B727/85 Main Landing Gear Side Strut 1/80
Applicability: All model 727 with line numbers 1 to 1361 inclusive. Document: 1. FAA AD 79-20-06, Amdt. 39-3581; or
2. Boeing SB No. 727-32-268, Rev. 1.
Compliance: As per requirement document No. 1.
Background: Incorrect parts may have been installed in the M-L-G side strut assemblies at manufacture.
Overview
The Civil Aviation Regulations 1998, specifically PART 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, was enacted to ensure that civil aviation operations in Australia meet the highest safety standards. This legislative instrument, issued by the Commonwealth of Australia, addresses the problem of ensuring the airworthiness of aircraft, particularly focusing on the Boeing 727 Series Aeroplanes. The regulation aims to rectify potential safety issues by mandating compliance with directives that ensure critical components, such as the main landing gear side strut, are installed correctly. The policy objective is to maintain and enhance the safety of civil aviation through rigorous oversight and enforcement of airworthiness standards.
The specific directive AD/B727/85 concerns the main landing gear side strut of Boeing 727 series aeroplanes, applicable to all models with line numbers 1 to 1361 inclusive. The directive was introduced in response to the potential installation of incorrect parts during manufacture, as evidenced by FAA AD 79-20-06, Amendment 39-3581, and Boeing Service Bulletin No. 727-32-268, Revision 1. Compliance with these documents ensures that any identified discrepancies are addressed to prevent safety hazards.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, applies to all Boeing 727 Series Aeroplanes with line numbers 1 to 1361 inclusive. This regulation mandates compliance with either FAA AD 79-20-06, Amendment 39-3581, or Boeing Service Bulletin No. 727-32-268, Revision 1, concerning the main landing gear side strut. The scope of the Act extends to ensuring that any discrepancies in the installation of components in the main landing gear side strut assemblies, which may have occurred during manufacture, are rectified to maintain airworthiness standards. The directive has a national jurisdictional reach and applies to all relevant aircraft registered within Australia, operated by Australian entities, or entering Australian airspace, thereby ensuring compliance with international civil aviation safety standards. No specific exclusions or exemptions are mentioned in the text, implying that all applicable aircraft must adhere to the directive unless otherwise specified by CASA.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, under the Civil Aviation Safety Authority's Schedule of Airworthiness Directives for Boeing 727 Series Aeroplanes, includes AD/B727/85, which addresses the main landing gear side strut (section 1/80). This directive applies to all Boeing 727 models with line numbers 1 to 1361 inclusive. The compliance requirements are detailed in FAA AD 79-20-06, Amendment 39-3581, or Boeing Service Bulletin No. 727-32-268, Revision 1. The directive was issued due to the potential installation of incorrect parts in the main landing gear side strut assemblies during manufacture.
The key provisions of this directive require operators of the specified Boeing 727 models to ensure that the main landing gear side struts comply with the specified requirements. This includes conducting a thorough inspection of the main landing gear side struts to verify the correct parts are installed and that there is no damage or deterioration. If any discrepancies are found, the operator must take corrective action by replacing or repairing the affected parts as per the specified documentation. Operators must also keep records of these inspections and any actions taken to comply with the directive.
Operators of the affected Boeing 727 models are required to ensure that their maintenance and inspection procedures are aligned with the directives outlined in FAA AD 79-20-06, Amendment 39-3581, and Boeing SB No. 727-32-268, Revision 1. This includes ensuring that all maintenance personnel are adequately trained and informed about the directive's requirements. Operators must also conduct regular inspections and maintain detailed records of all inspections and any corrective actions taken. Failure to comply with these requirements can lead to significant safety risks and may result in enforcement actions by the Civil Aviation Safety Authority.
Failure to comply with the provisions of AD/B727/85 can result in severe penalties. Under the Civil Aviation Act 1988, non-compliance with an airworthiness directive can lead to civil penalties, including fines of up to $202,000 for corporations and $40,400 for individuals. Additionally, non-compliance can result in criminal charges, where the penalties include fines of up to $2,020,000 for corporations and $404,000 for individuals, and imprisonment for up to five years. These stringent penalties underscore the importance of adhering to the directive to ensure the safety and airworthiness of the Boeing 727 aircraft.