Commonwealth legislation

AD/B727/106 - Main Landing Gear Support Link

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Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

4/10 complexity

This Airworthiness Directive makes compliance with FAA AD 88-24-01 (paras A–C) mandatory for specified Boeing 727s, requiring inspections and corrective work on the main landing‑gear support link shaft. It affects aircraft owners/operators and maintenance organisations, who must obtain the FAA AD, perform and record the required inspections/repairs, and bear associated costs. The measure aims to detect and remedy corrosion/cracking that could damage the wing or hydraulic system.

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AD/B727/106 - Main Landing Gear Support Link

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source Boeing 727 Series Aeroplanes

AD/B727/106 Main Landing Gear Support Link 3/89

Applicability: All models listed in Boeing SB 727-32-306.

Requirement: Action in accordance with the requirements of FAA AD 88-24-01 paras A, B and C. Compliance: In accordance with the Requirement document.

Background: There have been reports of corrosion and cracking of the support link shaft, failure of which, could cause damage to the wing and/or hydraulic system.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.