1AD/T53/2 - First Stage Power Turbine Rotor Blade Retaining Pins Retirement Life

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 

Image unavailable in extracted text 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.