Document ID: chunk:federal_register_of_legislation:F2006B09083:body:0
Version: federal_register_of_legislation:F2006B09083
Segment Type: other
Provision Reference: 
Character Range: 0–648

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

 DHC-3 (Otter) Series Aeroplanes

AD/DHC-3/33 Wing Strut to Fuselage Tie Bar 13/87

 Applicability: All models.

 Requirement: Action in accordance with de Havilland Canada SB 3/37 Rev B.

            Note: Canadian AD CF-82-26 refers.

            Compliance: Prior to the initial issue of a Certificate of Airworthiness and thereafter at periods not exceeding 12 months.

            Background: Tie bar lugs have been found corroded as well as the internal channel section under the cabin floor.