AD/ENST 28/8 - Fuselage Structure - Inspection

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

Legislation au F2006B09598 Not 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 28/8 Fuselage Structure - Inspection 10/73

Applicability: All models.

 

Requirement: Visually inspect for cracks the fuselage structure in the vicinity of the main rotor transmission assembly attachment.

 

Compliance: Within 50 hours time in service after 17 October 1975 and thereafter at intervals not exceeding 100 hours time in service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.