Document ID: chunk:federal_register_of_legislation:F2006B10210:body:0
Version: federal_register_of_legislation:F2006B10210
Segment Type: other
Provision Reference: 
Character Range: 0–1233

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

 GAF N22 and N24 Series Aeroplanes

 AD/GAF-N22/61
 Amdt 1

 Trim Tab Hinge 6/91

            Applicability: Nomad series aircraft with S/Nos N22S-159 to N22S-165 inclusive, incorporating Mod N663.

 Requirement: Action in accordance with ASTA Nomad Alert SB ANMD-55-25 Parts 1 and 2.

            Compliance: For Part 1. In accordance with initial issue of this Directive: Prior to exceeding 10 hours time in service after 6 June 1990.

            For Part 2. In accordance with initial issue of this Directive: Prior to exceeding 200 hours time in service after 6 June 1990.

            The effective date of this amendment is 13 June 1991.

            Background:  A condition may exist where the trim tab position of the horizontal stabilizers is incorrect, leading to a possibility of binding and overstress of the trim tab linkage with the stabilizer and trim setting at certain positions.

            This Amendment is raised to introduce a Revision of the Requirement document, which issues the accomplishment instructions for Part 2; replacement of the trim tab hinge.