Document ID: chunk:federal_register_of_legislation:F2006B10717:body:0
Version: federal_register_of_legislation:F2006B10717
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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 369/54 Governor Lever Control Rod - Replacement 3/82

 Applicability: All models.

            Requirement: Remove P/N 369A7706-3 RPM Governor Lever Control Rod and replace with P/N 369A7706-5 RPM Governor Lever Control Rod.

            Note: FAA AD 82-01-18, Amendment 39-4292, Hughes SIN No. DN-87 and SIN No. HN-169 also refer to this subject.

 Compliance: Within 25 hours time in service after 25 January 1982.

            Background: Failure of the aluminium control rod will result in loss of engine power control. The replacement rod is fabricated from steel.