AD/SD3-30/30 - Fin to Tailplane Attachment Bolts and Upper Shear Angle
1AD/SD3-30/30 - Fin to Tailplane Attachment Bolts and Upper Shear Angle
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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/SD3-30/30 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.