AD/ENST 28/7 Amdt 1 - Main Rotor Transmission Attachment Bolts - Inspection and Replacement

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

Legislation au F2006B09597 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 28/7

Amdt 1

Applicability: All models.


Main Rotor Transmission Attachment Bolts - Inspection and Replacement


4/77

 

Requirement: 1. Inspect the 4 bolts attaching the main rotor transmission assembly to the fuselage frame for a torque preloading of 100-110 inch pounds.

 

2. Modify the attachment of the main rotor transmission assembly to fuselage attachment as per Enstrom Service Information Letter No. 0057.

 

Compliance: For Para. 1: At intervals not exceeding 50 hours time in service until modified and then once only within 100 hours time in service after modification as per SIL No. 0057.

 

For Para. 2: Modify within 300 hours time in service after 1 June 1977.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.