Document ID: chunk:federal_register_of_legislation:F2006B06792:body:0
Version: federal_register_of_legislation:F2006B06792
Segment Type: other
Provision Reference: 
Character Range: 0–658

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

 Short SC7 (Skyvan) Series Aeroplanes

AD/SC7/17 Outer Flap - Replacement of Lifed Items
                   and Reinforcement of Flap Structure

 Applicability: All Skyvan series 3, 3A and 3M. Document:  Short SB No. 57-62.
 Compliance: As detailed in the requirement document.

7/80

            Background: Retirement of hinge arms and operating arms, and reinforcement of the flap structure, are required as part of the life extension modification and to ensure the continued airworthiness of the flaps.