Document ID: chunk:federal_register_of_legislation:F2006B10653:body:0
Version: federal_register_of_legislation:F2006B10653
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Schweizer (Hughes) 269 Series Helicopters

AD/HU 269/95 Cyclic Pitch Control 7/90 DM

 Applicability: All model 269C helicopters S/N 0004 thru 1456.

            Requirement: Unless previously accomplished, action in accordance with Schweizer Service Bulletin B-237.

            Note: FAA Emergency AD 90-09-07 refers.

 Compliance: Prior to 18 May 1990.

            Background: The manufacturer has advised that movement of the lower longitudinal cyclic control rod spring attachment clamp, P/N AN735-9, has occurred. Movement of this clamp could restrict cyclic control which could result in loss of helicopter control.