Document ID: chunk:federal_register_of_legislation:F2006B09570:body:0
Version: federal_register_of_legislation:F2006B09570
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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 28/15
 Amdt 2

 Tail Rotor Spindle and Drive Shaft - Inspection and Retirement

 8/77

 Applicability: All models F-28 and 280.

             Requirement: 1. Remove tail rotor spindles P/N 28-15202 from service and replace with a new spindle P/N 28-15202-13 or a re- worked spindle which may be identified by an 8- character serial number acid etched on the outside of the spindle centre section.

2.    Install tail rotor strike tabs in accordance with Enstrom Service Directive Bulletin No. 0037 Revision A or FAA AD 77-04-04 Amendment 39-2839.

             3.    Inspect the tail rotor spindle in accordance with the above Bulletin or FAA AD.

4.    Inspect the tail rotor drive shaft in accordance with Enstrom ServiceDirective Bulletin No. 0039.

 Compliance: For Para. 1 - Within 10 hours time in service after 17 August 1977.

            For Para. 2 - Forthwith.

            For Para. 3 and 4 - Before further flight following any tail rotor strike.