Document ID: chunk:federal_register_of_legislation:F2006B10391:body:0
Version: federal_register_of_legislation:F2006B10391
Segment Type: other
Provision Reference: 
Character Range: 0–1001

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

 British Aerospace BAe 125 Series Aeroplanes

 AD/HS 125/113
 Amdt 1

       MLG Side Stay Arm Assemblies and Torque Links

 5/98

 Applicability: Series 800A and 800B.

 Requirement: Action in accordance with BAe SB 32-227. Compliance: Prior to 30 November 1990.
            The compliance of the original issue of this directive remains unchanged. This amendment becomes effective on 23 April 1998.
            Background: Damage and cracks in main landing gear side stay have been reported to manufacturer. If not detected these could lead to landing gear failure. This requirement is mandatory in Country of origin.

            Amendment 1 is issued to re-instate this directive to the series.

            The original issue of this Airworthiness Directive became effective on 30 November 1990.

                   1