COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Boeing 727 Series Aeroplanes
AD/B727/29 Flight Spoiler Actuator Support Fitting - Inspection and Replacement
7/66
Applicability: All models. Document: Boeing SB No. 57-71. Compliance: Forthwith.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serves as the overarching regulatory framework governing civil aviation safety and operations within the country. One particular legislative instrument under this framework is F2006B02729, which amends the regulations to address specific safety concerns regarding Boeing 727 series aeroplanes. This instrument was introduced to rectify a problem identified with the flight spoiler actuator support fitting, necessitating immediate inspection and replacement as outlined in Boeing Service Bulletin No. 57-71. The policy objective behind this regulation is to ensure the ongoing airworthiness of Boeing 727 aeroplanes by mandating critical maintenance actions to prevent potential safety hazards. This amendment aims to uphold the high standards of safety and reliability within Australia's civil aviation sector, aligning with broader regulatory goals set forth by the Civil Aviation Safety Authority.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39 - 105, specifically addresses the safety of Boeing 727 Series aeroplanes through Airworthiness Directives, with AD/B727/29 being one such directive. This particular directive applies to all models of Boeing 727 aeroplanes and mandates an inspection and replacement of the flight spoiler actuator support fitting. Compliance with this directive is required forthwith, as specified in Boeing Service Bulletin No. 57-71, ensuring that all applicable aircraft meet the necessary safety standards. The directive applies nationally across the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority, and is integral to maintaining the airworthiness of Boeing 727 aircraft operating within Australian airspace. The scope of the directive encompasses the inspection and, if necessary, the replacement of the specified component to ensure continued compliance with safety regulations, with no stated exclusions or exemptions within the text provided.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39, include specific provisions related to the airworthiness directives for various aircraft, such as the Boeing 727 series aeroplanes. In particular, AD/B727/29 focuses on the flight spoiler actuator support fitting, mandating inspections and replacements to ensure continued safe operation of these aircraft (Section 39-105). The directive applies to all models of the Boeing 727 series and is based on Boeing Service Bulletin No. 57-71. Compliance with these directives is required immediately, ensuring that all necessary actions are taken without delay (Section 39-105).
The Act imposes several obligations on the parties or entities governed by these provisions. Firstly, it requires aircraft operators to conduct a thorough inspection of the flight spoiler actuator support fitting on all Boeing 727 series aeroplanes as specified in Boeing SB No. 57-71. This includes verifying the condition of the support fitting and ensuring it is free from any defects or damage that could compromise the safety of the flight. If any issues are identified, the operators must take appropriate corrective action, which may include replacing the support fitting, to ensure compliance with the airworthiness directives (Section 39-105).
Failure to comply with the airworthiness directives outlined in AD/B727/29 can result in significant consequences. The Act stipulates that non-compliance with these directives may lead to various civil and criminal penalties. Civil penalties can include fines and potential grounding of the aircraft until the required actions are taken. In severe cases, non-compliance may also result in criminal charges, with penalties potentially including imprisonment for individuals found responsible for failing to adhere to these critical safety regulations. The specific penalties and consequences are determined based on the severity of the non-compliance and any resultant safety risks (Section 39-105).