Document ID: chunk:federal_register_of_legislation:F2006B06832:body:0
Version: federal_register_of_legislation:F2006B06832
Segment Type: other
Provision Reference: 
Character Range: 0–671

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

 Short SD3-30 Series Aeroplanes

 AD/SD3-30/30 Fin to Tailplane Attachment Bolts
                          and Upper Shear Angle

 7/95
 DM

 Applicability: All models.

 Requirement: Action in accordance with Shorts Service Bulletin SD330-55-18.

            Compliance: Within 60 days after 03 May 1995; thereafter at intervals not exceeding 1500 hours time in service.

            Background:  Fin to tailplane attach bolts have been found loose, and rivets in the upper shear angle have been found pulled or loose.