AD/ENST 28/29 - Rotor Head Hub

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

Legislation au F2006B09585 Not in force Legislative Instrument

Legislation content

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 28/29 Rotor Head Hub  12/86 TX

 

Applicability: All models.

 

Requirement: 1. Inspect the upper and lower rotor head hub plates in accordance with Enstrom Service Directive Bulletin No. 0072 Paragraph A.

 

2. Inspect the upper and lower hub plates and other hub components in accordance with Enstrom Service Directive Bulletin No. 0072 Paragraph C.

 

Compliance: For Para 1: Within 25 hours time in service after 31 October 1986 and thereafter at intervals not exceeding 50 hours time in service.

 

For Para 2: Within 25 hours time in service after 31 October 1986 for helicopters known to have experienced blade strikes, sudden stoppages or heavy landings.

 

Background: The manufacturer has received three reports of cracking in the upper and lower hub plates.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Interactions

Authorises

All Versions

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.