AD/T53/2 - First Stage Power Turbine Rotor Blade Retaining Pins Retirement Life

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

Legislation au F2006B07249 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


AlliedSignal (Lycoming) Turbine Engines - T53 Series

 

AD/T53/2 First Stage Power Turbine Rotor Blade

Retaining Pins Retirement Life


1/86

 

Applicability: T5313A, T5313A S/N Suffix "A", T5313B S/N LEO7500 to LEO7513 and LEO7528 to LEO7532. T53-L-13, T53-L-13 S/N Suffix "A" T53-L-13A and T53-L-13B S/N

prior to LE22568.

 

Document: 1. Lycoming Product Support Service Bulletin No. 0003, Rev. 5; or

 

2. AD/LYC-T/5B. Compliance: 30 November 1973.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.