Document ID: chunk:federal_register_of_legislation:F2006B06834:body:0
Version: federal_register_of_legislation:F2006B06834
Segment Type: other
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Character Range: 0–730

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

 Short SD3-30 Series Aeroplanes

AD/SD3-30/32 Inner Flap Sub-Assembly Lever Bracket 5/97

 Applicability: All SD3-30 aircraft.

 Requirement: Inspect in accordance with Shorts Mandatory Service Bulletin SD3-27-36.

            Compliance: Before 27 July 1997 for the initial inspection; thereafter as specified in the Requirement Document for the repeat inspection periods.

            This Airworthiness Directive becomes effective on 24 April 1997.

            Background: The manufacturer received reports of corrosion and cracking on inner flap sub- assembly lever brackets.