Document ID: chunk:federal_register_of_legislation:F2006B02497:body:0
Version: federal_register_of_legislation:F2006B02497
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Eurocopter AS 355 (Twin Ecureuil) Series Helicopters

 AD/AS 355/43
 Amdt 1

 In Door Sliding Windows 3/94

            Applicability: Models E, F, F1, F2, and N, equipped with the sliding windows listed in the Requirement Document.

 Requirement: Action in accordance with Eurocopter AS 355 SB 05.26R1.

            Note: DGAC AD 93-089-048(B) R1 refers.

             Compliance: 1. Inspect within 25 hours time in service after 3 March 1994, and thereafter at intervals not exceeding 25 hours time in service until modified.

             2. Modify within 100 hours time in service after 3 March 1994, and thereafter inspect at intervals not exceeding 100 hours time in service until replaced by the post mod. windows listed in paragraph 1.C.3 of the Requirement Document.

            Note: Both the Requirement Document and the DGAC AD call the modification of the undamaged windows a Repair.

            The effective date of the initial issue of this Directive was 7 July 1993.

            Background:  This Directive is raised to preclude the loss of a window during flight. Amendment 1 introduces a modification to existing windows in lieu of automatic window replacement.