NSN 2840-01-117-2903

Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE

2840-01-117-2903 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: 9653M35P24, 9653M35P21, 9397M51P01, 1999M69P06, 1999M69P03, 1999M69P02, 2840-01-117-2903, 01-117-2903, 2840011172903, 011172903

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
28AUG 12, 198101-117-290350531 ( BLADE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-117-2903
Part Number Cage Code Manufacturer
9653M35P2407482GENERAL ELECTRIC COMPANYDBA GE
9653M35P2107482GENERAL ELECTRIC COMPANYDBA GE
9397M51P0107482GENERAL ELECTRIC COMPANYDBA GE
1999M69P0607482GENERAL ELECTRIC COMPANYDBA GE
1999M69P0307482GENERAL ELECTRIC COMPANYDBA GE
1999M69P0207482GENERAL ELECTRIC COMPANYDBA GE
Technical Data | NSN 2840-01-117-2903
Characteristic Specifications
DESIGN TYPE COMPRESSOR
ENGINE SECTION LOCATION LOW PRESSURE COMPRESSOR
STAGE NUMBER2
OVERALL LENGTH30.814 INCHES MINIMUM AND 30.834 INCHES MAXIMUM
OVERALL WIDTH3.397 INCHES NOMINAL
MATERIAL THICKNESS0.230 INCHES MINIMUM AND 0.561 INCHES MAXIMUM
DIAMETER31.305 INCHES NOMINAL
SPECIAL FEATURESORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
CRITICALITY CODE JUSTIFICATIONAGAV
END ITEM IDENTIFICATIONACFT.ENG. TF39