AD/SD3-30/32 - Inner Flap Sub-Assembly Lever Bracket
1AD/SD3-30/32 - Inner Flap Sub-Assembly Lever Bracket
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.