Product Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE

2840-00-256-1113 A single stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud.

Part Alternates: 536751CL22, 665951CL22, 799351CL22, 2840-00-256-1113, 00-256-1113, 2840002561113, 002561113

Engines, Turbines, and Components | Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Supply Group (FSG) NSN Assign. NIIN
28 00-256-1113

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Technical Data | NSN 2840-00-256-1113

Characteristic Specifications
MATERIAL NICKEL ALLOY VANE
MATERIAL DOCUMENT AND CLASSIFICATION PWA653 ASSN STD SINGLE MATERIAL RESPONSE VANE
ENGINE SECTION LOCATION TURBINE
SPECIAL FEATURES ORIGINAL NAME VANE,TURBINE NOZZLE,TURBINE ENGINE
CRITICALITY CODE JUSTIFICATION AGAV
III END ITEM IDENTIFICATION TF-33 AIRCRAFT ENGINE

Restrictions/Controls & Freight Information | NSN 2840-00-256-1113

Category Code Description
Hazardous Material Indicator CodeNThere is no data in the HMIS and the NSN is in an FSC not generally suspected of containing hazardous materials
Category Code Description
No Freight Information