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.