Document ID: chunk:federal_register_of_legislation:F2006B09571:body:0
Version: federal_register_of_legislation:F2006B09571
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Enstrom F-28 Series Helicopters

 AD/ENST 28/16 Tail Rotor Pitch Link Retainer and
                         Guide Bolt - Replacement

 10/77

            Applicability: Models F-28C and 280C fitted with the Wide Cord tail rotors and S/Nos. as listed in the requirement document.

             Requirement: 1. Inspect the P/N 28-16320 pitch link retainer in accordance with Enstrom Service Directive Bulletin No. 0040.

             2. Replace the P/N 28-16320 pitch link retainer and guide bolts in accordance with Enstrom Service Directive Bulletin No. 0040 and 0043.

            FAA AD 77-15-04 refers.

             Compliance: 1. For Part 1 of the requirement document - before each flight, until part 2 is complied with.

             2. For Part 2 of the requirement document - within 100 hours time in service after 30 November 1977.