Document ID: chunk:federal_register_of_legislation:F2006B06872:body:0
Version: federal_register_of_legislation:F2006B06872
Segment Type: other
Provision Reference: 
Character Range: 0–711

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

 Short SD3-60 Series Aeroplanes

 AD/SD3-60/28 Horizontal Stabilizer - Rear Spar Web/Boom 7/88

DM

 Applicability: All models with S/Nos SH3601 to SH3691 and SH3694. Requirement:  Action in accordance with Shorts SB SD360-55-16.
            Compliance: Unless already accomplished, prior to 31 July 1988 and thereafter as per Requirement Document until modified in accordance with Shorts SB SD360-55-12.

            Background:  Testing on a horizontal stabilizer with service usage has shown failure of some rivets connecting the rear spar web to the booms.