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

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B06832 In force Legislative Instrument

Legislation content

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.