AD/JT8D/14 - First Stage Compressor Hub Blade Slots

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

Legislation au F2006B10976 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Pratt and Whitney Turbine Engines - JT8D Series

 

AD/JT8D/14 First Stage Compressor Hub Blade Slots 2/84

Applicability: JT8D-9, -9A, -11, -15, -15A, -17, -17A, -17R, -17AR.

 

Document: 1. Pratt & Whitney Aircraft Alert SB No. 4841, Revision 6.

 

Note: FAA AD 78-17-02 R2 with subsequent amendments is listed for reference purposes only.

 

or

 

2. AD/PW-T/47 Amdt 6.

 

Compliance: As detailed in the Requirement Document.

 

Background:  This Directive is raised in issue to ensure compliance with the latest revision of the requirement document which adds to the effectivity listing those 'A' series engines that have, or will be, obtained by conversion.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.