Product Details | TURBINE ENGINE AXIAL COMPRESSOR ROTOR

2840-01-067-2124 All Except USA A single or multistage item consisting of a disk or series of disks fastened together on a drum or central shaft or a series of curved blades mounted on an integral part of the disk(s), set at an angle and extending radially from the disk, or extending from the axis of rotation to the rim of the disk. It is designed to impart energy of motion to the air between the blade surfaces in an axial direction in the compressor section of a turbine engine.20228350096Gas Turbines and Jet Engines; Non-Aircraft Prime Mover, Aircraft Non-Prime Mover, and Components28400068Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Part Alternates: 728613, 2840-01-067-2124, 01-067-2124, 2840010672124, 010672124

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

Supply Group (FSG) NSN Assign. NIIN
28 01-067-2124

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Restrictions/Controls & Freight Information | NSN 2840-01-067-2124

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