AD/JT8D-200/3 - Low Pressure Turbine Anti-Rotation Pins

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Legislation au F2006B11001 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-200 Series

 

AD/JT8D-200/3 Low Pressure Turbine Anti-Rotation Pins 10/92

Applicability: JT8D-209, -217, -217A, -217C and -219 turbofan engines.

Requirement: As detailed in the technical requirements of FAA Airworthiness Directive 88-04-02. Compliance:              As detailed in the Requirement document, with an effective date of 17 September

1992.

 

Background:  This Directive requires inspection, replacement and modification of the low pressure turbine anti-rotation pins.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.