AD/BELL 47/72 Amdt 2 - Main Rotor Hub Core P/N 47-120-117-1

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

Legislation au F2006B04698 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

 


Bell Helicopter Textron 47 (All Variants) Series Helicopters

 

AD/BELL 47/72

Amdt 2


Main Rotor Hub Core P/N 47-120-117-1 3/87

 

Applicability: All model 47 series fitted with P/N 47-120-117-1 hub core.

 

Requirement: Irrespective of the dimensional exclusion given in Part I of Bell SB 47-04-1-73-2, inspect in accordance with Part II of the document.

 

Compliance: At each issue of a new Maintenance Release, for all cores which have exceeded 1200 hours total time-in-service or for which the total time in service is unknown.

 

Background: A crack has been found in the web of a hub core which is exempted by dimensional criteria from the requirement for visual inspection at 100 hourly periods. Amendment 1 included all P/N 47-120-117-1 cores. This amendment brings the compliance periodicity into line with the inspection interval for Maintenance Release.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.