AD/ENST 28/24 - Main Rotor Retention Assembly - Inspection

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B09580 In force Legislative Instrument

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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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.