NSN 2840-01-187-3182

Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK

2840-01-187-3182 An item having provisions on the outer periphery for attaching a designated number of BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It also has provisions for attachment to a HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE and/or a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE.

Alternate Parts: 9940M55P18, 9940M55P13, 9940M55P08108, 9940M55P08-108, 2116M23P01, 1590M59P01, 9940M55P18, 9940M55P13, 9940M55P08108, 9940M55P08-108, 1590M59P01, 2840-01-187-3182, 01-187-3182, 2840011873182, 011873182

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
28AUG 21, 198401-187-318250567 ( DISK, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-187-3182
Part Number Cage Code Manufacturer
9940M55P1858828CFM INTERNATIONAL, INC.
9940M55P1358828CFM INTERNATIONAL, INC.
9940M55P08-10858828CFM INTERNATIONAL, INC.
2116M23P0158828CFM INTERNATIONAL, INC.
1590M59P0158828CFM INTERNATIONAL, INC.
9940M55P1807482GENERAL ELECTRIC COMPANYDBA GE
9940M55P1307482GENERAL ELECTRIC COMPANYDBA GE
9940M55P08-10807482GENERAL ELECTRIC COMPANYDBA GE
1590M59P0107482GENERAL ELECTRIC COMPANYDBA GE
Technical Data | NSN 2840-01-187-3182
Characteristic Specifications
DESIGN TYPE AXIAL COMPRESSOR
ENGINE SECTION LOCATION COMPRESSOR
STAGE NUMBER3
OVERALL WIDTH1.180 INCHES MINIMUM AND 1.190 INCHES MAXIMUM
MATERIAL THICKNESS1.5000 INCHES NOMINAL
DIAMETER17.000 INCHES NOMINAL
SPECIAL FEATURESORIGINAL NAME DISK,TURBINE,TURBINE ENGINE
REFERENCE DATA AND LITERATURE2J-F108-14 FIG 72-31-00-1 IND 120D
END ITEM IDENTIFICATIONACFT ENG F108
PART NAME ASSIGNED BY CONTROLLING AGENCYDISK,COMPRESSOR ROTOR - STAGE 3