Document ID: chunk:federal_register_of_legislation:F2006B02629:body:0
Version: federal_register_of_legislation:F2006B02629
Segment Type: other
Provision Reference: 
Character Range: 0–629

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

 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.