Document ID: chunk:federal_register_of_legislation:F2006B10886:body:0
Version: federal_register_of_legislation:F2006B10886
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 British Aerospace BAe 3100 (Jetstream) Series Aeroplanes

                              AD/JETSTREAM/19 Cracking of MLG Cylinder Upper Attach Lug

 Applicability: As listed in the requirement document.

 Requirement: Action in accordance with British Aerospace SB 32-JA860812. Compliance:  In accordance with the requirement document.

5/87
            Background:  During fatigue testing of the main landing gear a crack occurred in the cylinder near the upper toggle attachment lug.