Document ID: chunk:federal_register_of_legislation:F2006B06892:body:0
Version: federal_register_of_legislation:F2006B06892
Segment Type: other
Provision Reference: 
Character Range: 0–778

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

 Short SD3-60 Series Aeroplanes

AD/SD3-60/46 Inner Flap Sub-Assembly Lever Bracket 7/97

 Applicability: All SD3-60 aircraft.

 Requirement: Inspect in accordance with Shorts Mandatory Service Bulletin SD360-27-26.

            Note: UK CAA AD 011-01-97 refers.

            Compliance: Unless already accomplished, before 19 September 1997 for the initial inspection; thereafter as specified in the requirement document.

            This airworthiness directive becomes effective on 19 June 1997.

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