Document ID: chunk:federal_register_of_legislation:F2006B09580:body:0
Version: federal_register_of_legislation:F2006B09580
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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 28/24 Main Rotor Retention Assembly - Inspection 10/82

 Applicability: All model F-28A, F-28C, F-28F, 280, 280C and 280F. Document:  Enstrom Service Directive Bulletin No. 0057.
            Note: FAA AD 82-16-09 Amdt. 39-4429 refers.

            Compliance: Within 100 hours time in service after 31 October 1982, and thereafter at intervals not exceeding 200 hours time in service.

            Background:  Manufacture reports misalignment of the nylon shims has worn grooves in the inner surfaces of the blade grip.