Document ID: chunk:federal_register_of_legislation:F2006B10731:body:0
Version: federal_register_of_legislation:F2006B10731
Segment Type: other
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters

AD/HU 369/67
 Amdt 1

 Applicability: All models.

 Main Rotor Retention Strap 4/88

            Requirement: Action in accordance with Part 1 of McDonnell Douglas SIN HN214, DN154, EN44 or FN33 as applicable.

 Compliance: As applicable by helicopter model, either:

(a)      within three months or one hundred hours time in service after the previous compliance with AD/HU 369/28D whichever occurs first; or

(b)     within nine months or three hundred hours time in service after the previous compliance with the initial issue of this Directive whichever occurs first;

 (c)      and thereafter in accordance with the Requirement document. Background: The manufacturer has consolidated the inspection within the single SIN.