Product Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE

2840-00-872-1030 An item mounted on a DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the compressor section of an ENGINE, GAS TURBINE, AIRCRAFT.

Part Alternates: 2840-00-872-1030, 00-872-1030, 2840008721030, 008721030

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

Supply Group (FSG) NSN Assign. NIIN
28 00-872-1030

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Technical Data | NSN 2840-00-872-1030

Characteristic Specifications
DESIGN TYPE COMPRESSOR
ENGINE SECTION LOCATION HIGH PRESSURE COMPRESSOR
STAGE NUMBER 2
SPECIAL FEATURES ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
CRITICALITY CODE JUSTIFICATION AGAV
III END ITEM IDENTIFICATION TF-41 AIRCRAFT ENGINE
MANUFACTURERS CODE 63005
DESIGN CONTROL REFERENCE 6863947

Restrictions/Controls & Freight Information | NSN 2840-00-872-1030

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