NSN 2840-01-106-2591

Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE

2840-01-106-2591 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: 111R111P23, 111R111P23, 111R111P23, 2840-01-106-2591, 01-106-2591, 2840011062591, 011062591

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
28JAN 14, 198101-106-259150531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-106-2591
Part Number Cage Code Manufacturer
111R111P233204ABLADES TECHNOLOGY LTD
111R111P23S0635BLADES TECHNOLOGY LTDDBA ISCAR BLADES LTD. - FORMERLY
111R111P2307482GENERAL ELECTRIC COMPANYDBA GE
Technical Data | NSN 2840-01-106-2591
Characteristic Specifications
DESIGN TYPE COMPRESSOR
ENGINE SECTION LOCATION LOW PRESSURE COMPRESSOR
STAGE NUMBER5
OVERALL LENGTH5.467 INCHES NOMINAL
SPECIAL FEATURESORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
CRITICALITY CODE JUSTIFICATIONAGAV
END ITEM IDENTIFICATIONACFT ENG J79