NSN 2840-01-139-2392

Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE ROTOR

2840-01-139-2392 A single or multistage assembly designed to receive thermal energy from the combustion section and convert it to mechanical energy to drive the ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or the ROTOR, FAN, AIRCRAFT GAS TURBINE ENGINE through a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of disks, blades, hubs, and the like. It is the moving part of a TURBINE ASSEMBLY, AIRCRAFT GAS TURBINE ENGINE. It has facilities for attaching to a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.

Alternate Parts: 9995M22G07, 9995M22G06, 9995M22G04, 9995M22G01, 9995M22G07, 9995M22G06, 9995M22G04, 9995M22G01, 2840-01-139-2392, 01-139-2392, 2840011392392, 011392392

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
28SEP 27, 198201-139-239250591 ( ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-139-2392
Part Number Cage Code Manufacturer
9995M22G0758828CFM INTERNATIONAL, INC.
9995M22G0658828CFM INTERNATIONAL, INC.
9995M22G0458828CFM INTERNATIONAL, INC.
9995M22G0158828CFM INTERNATIONAL, INC.
9995M22G0707482GENERAL ELECTRIC COMPANYDBA GE
9995M22G0607482GENERAL ELECTRIC COMPANYDBA GE
9995M22G0407482GENERAL ELECTRIC COMPANYDBA GE
9995M22G0107482GENERAL ELECTRIC COMPANYDBA GE
Technical Data | NSN 2840-01-139-2392
Characteristic Specifications
DESIGN TYPE AXIAL COMPRESSOR
ENGINE SECTION LOCATION COMPRESSOR
STAGE NUMBER9
SPECIAL FEATURESWAS COMPRESSOR ROTOR,AXIAL,TURBINE ENGINE; DUAL ROTORS,9 STAGES; HIGH BYPASS FAN
CRITICALITY CODE JUSTIFICATIONAGAV
END ITEM IDENTIFICATIONACFT ENG F108-CF-100