NSN 2840-01-106-2597

Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE

2840-01-106-2597 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.

Alternate Parts: 111R113P26, 111R113P26, 111R113P26, 111R113P26, 2840-01-106-2597, 01-106-2597, 2840011062597, 011062597

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
28JAN 14, 198101-106-259750531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-106-2597
Part Number Cage Code Manufacturer
111R113P263204ABLADES TECHNOLOGY LTD
111R113P26S0635BLADES TECHNOLOGY LTDDBA ISCAR BLADES LTD. - FORMERLY
111R113P2607482GENERAL ELECTRIC COMPANYDBA GE
111R113P2633404TRW INC TRW COMPRESSOR COMPONENTS
Technical Data | NSN 2840-01-106-2597
Characteristic Specifications
DESIGN TYPE COMPRESSOR
ENGINE SECTION LOCATION HIGH PRESSURE COMPRESSOR
STAGE NUMBER11
OVERALL LENGTH2.436 INCHES MINIMUM AND 2.438 INCHES MAXIMUM
OVERALL WIDTH0.390 INCHES NOMINAL
SPECIAL FEATURESORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
CRITICALITY CODE JUSTIFICATIONAGAV
END ITEM IDENTIFICATIONACFT ENG J79