AD/B727/58 Amdt 1 - Main Landing Gear Actuator Beam Support Link - Inspection and Modification

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Legislation au F2006B02760 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Boeing 727 Series Aeroplanes

 

AD/B727/58

Amdt 1


Main Landing Gear Actuator Beam Support Link - Inspection and Modification


9/71

 

Applicability: All models.

 

Requirement: Inspect the main landing gear actuator beam support link P/N 65-19657-4, -5 or -8 in accordance with Boeing SB No. 32-90 Rev. 2 and link P/N 65-19657-13 in accordance with Boeing SB No. 32-189 until replaced by link P/N 65-19657-11.

 

Compliance: Forthwith.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Safety Authority (CASA) established the Civil Aviation Regulations 1998 to regulate the aviation industry in Australia and ensure the safety of all aviation activities within the country. One of the specific instruments under these regulations is the Schedule of Airworthiness Directives, which provides mandatory safety instructions and maintenance requirements for various aircraft types. The Boeing 727 Series Aeroplanes, for example, are subject to specific directives to maintain their airworthiness and safety standards. One such directive, AD/B727/58 Amendment 1, focuses on the inspection and modification of the main landing gear actuator beam support link to address potential safety issues and ensure the continued safe operation of these aircraft. The directive mandates inspections and modifications according to specified Boeing service bulletins and parts, aiming to enhance the reliability and safety of the aircraft's landing gear system.

Scope and Application

The Civil Aviation Safety Authority’s Schedule of Airworthiness Directives, specifically AD/B727/58 Amendment 1, applies to all Boeing 727 series aeroplanes. This regulation mandates that operators and maintainers of Boeing 727 aircraft must inspect and modify the main landing gear actuator beam support link components in accordance with the specified Boeing Service Bulletins until they are replaced by the updated part number 65-19657-11. Compliance with these directives is required immediately, ensuring that all affected parts are inspected and modified without delay to maintain the airworthiness of the aircraft. The scope of this regulation is confined to the specific components listed, and it does not extend to other parts of the aircraft unless subsequently covered by additional directives. The authority to enforce these directives is vested in the Civil Aviation Safety Authority under the Civil Aviation Regulations 1998, and any further clarification or extension of these directives may be provided through subsequent legislative instruments or amendments.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, specifically Part 39 - 105 and the Schedule of Airworthiness Directives (AD/B727/58 Amendment 1), pertain to the inspection and modification of the main landing gear actuator beam support link for Boeing 727 series aeroplanes. Section 39.105 sets out the overarching framework for airworthiness directives, while the specific AD/B727/58 Amendment 1 mandates detailed inspection and modification procedures for certain parts of the main landing gear actuator beam support link (sections 39.105.10(a) and (b)). These sections require inspecting parts P/N 65-19657-4, -5, or -8 in accordance with Boeing Service Bulletin (SB) No. 32-90 Rev. 2, and parts P/N 65-19657-13 in accordance with Boeing SB No. 32-189, until these are replaced by parts P/N 65-19657-11. The obligations and requirements imposed by this legislation are precise and time-sensitive. Operators of Boeing 727 series aeroplanes must ensure that the specified inspection and modification procedures are carried out immediately, as indicated by the term "forthwith" in the directive. This means that inspections and any necessary modifications must be completed without delay, ensuring that the aircraft remains airworthy. Operators must adhere to the guidance provided in the referenced Boeing service bulletins, which detail the specific inspection methods and criteria for compliance. Additionally, operators must keep accurate records of all inspections and modifications to demonstrate compliance with the airworthiness directive. Failure to comply with the provisions of AD/B727/58 Amendment 1 can result in significant consequences. Under the Civil Aviation Act 1988, non-compliance with an airworthiness directive can lead to civil penalties, including fines up to the statutory maximum of $126,000 for individuals and $630,000 for corporations, as well as potential criminal charges. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement action against operators who fail to comply with airworthiness directives, which could include grounding the aircraft, suspension of operations, or other regulatory measures. Additionally, non-compliance could result in safety risks, leading to potential accidents or incidents that could endanger lives and property.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.