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Features & Benefits
Extracts kinetic energy from high-velocity gas streams for optimal performance
Facilitates the expansion of heated air to generate rotary shaft power
Engineered to maintain uniform axial velocity under extreme mechanical stress
Critical component for the Rolls-Royce T56 turboprop engine
Fabricated from corrosion-resistant steel for enhanced durability
Specifications
Engine Section Location: Turbine
End Item Identification: T-56-15, C-130 Aircraft
Material: Steel Corrosion Resisting Blade
Technical Information
NIIN
012800705
NSN
2840-01-280-0705
FSCG
2840
FSCG Category
Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components
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