Product Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE

2840-01-107-2088 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: 6021T14P07, 2840-01-107-2088, 01-107-2088, 2840011072088, 011072088

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

Supply Group (FSG) NSN Assign. NIIN
28 01-107-2088

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Technical Data | NSN 2840-01-107-2088

Characteristic Specifications
MATERIAL STEEL BLADE
DESIGN TYPE COMPRESSOR
ENGINE SECTION LOCATION LOW PRESSURE COMPRESSOR
STAGE NUMBER 4
OVERALL LENGTH 2.218 INCHES NOMINAL
OVERALL WIDTH 0.557 INCHES NOMINAL
SPECIAL FEATURES ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
CRITICALITY CODE JUSTIFICATION AGAV
III END ITEM IDENTIFICATION ACFT ENG TF34
MANUFACTURERS CODE 99207
DESIGN CONTROL REFERENCE 6021T14P07

Restrictions/Controls & Freight Information | NSN 2840-01-107-2088

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