Document ID: chunk:federal_register_of_legislation:F2006B09040:body:0
Version: federal_register_of_legislation:F2006B09040
Segment Type: other
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Character Range: 0–859

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

 DHC-2 (Beaver) Series Aeroplanes

 AD/DHC-2/22
 Amdt 1

 Aileron Centre Hinge Bracket 1/88 DM

            Applicability: All models DHC-2 Mk1 and MkII and DHC-2 MkIII. Turbo- Beaver Aircraft not incorporating Modification 2/1536.

 Requirement: Modify in accordance with De-Havilland Canada S.B 2/37 Rev C.

            Note: Canadian AD CF-84-02-R1 refers.

            Compliance: Unless already accomplished within 200 hours time in service after 19 November 1987 or prior to 19 January 1988 whichever is earlier.

            Background:  The initial issue of this Directive allowed an open ended continued inspection. However, due to failure of a cast bracket in flight this option is now terminated.