Federal Register of Legislation
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.
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