NSN 2840-01-433-2711

Part Details | AIRCRAFT GAS TURBINE ENGINE FAN BLADE

2840-01-433-2711 An item mounted on a DISK, FAN, AIRCRAFT GAS TURBINE ENGINE. It is designed to create the flow of air in the fan section of a ENGINE, GAS TURBINE, AIRCRAFT.

Alternate Parts: 2113M18P03, 2113M18P01, 1999M69P09, 1999M69P08, 1999M69P07, 1999M69P01, 1782M54P01, 1782M53G05, 1782M53G04, 1782M53G03, 1782M53G02, 1782M53G01, 2840-01-433-2711, 01-433-2711, 2840014332711, 014332711

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
28JUN 25, 199601-433-271150533 ( BLADE, FAN, AIRCRAFT GAS TURBINE ENGINE )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-433-2711
Part Number Cage Code Manufacturer
2113M18P0307482GENERAL ELECTRIC COMPANYDBA GE
2113M18P0107482GENERAL ELECTRIC COMPANYDBA GE
1999M69P0907482GENERAL ELECTRIC COMPANYDBA GE
1999M69P0807482GENERAL ELECTRIC COMPANYDBA GE
1999M69P0707482GENERAL ELECTRIC COMPANYDBA GE
1999M69P0107482GENERAL ELECTRIC COMPANYDBA GE
1782M54P0107482GENERAL ELECTRIC COMPANYDBA GE
1782M53G0507482GENERAL ELECTRIC COMPANYDBA GE
1782M53G0407482GENERAL ELECTRIC COMPANYDBA GE
1782M53G0307482GENERAL ELECTRIC COMPANYDBA GE
1782M53G0207482GENERAL ELECTRIC COMPANYDBA GE
1782M53G0107482GENERAL ELECTRIC COMPANYDBA GE
Technical Data | NSN 2840-01-433-2711
Characteristic Specifications
DESIGN TYPE AXIAL COMPRESSOR
ENGINE SECTION LOCATION FAN
STAGE NUMBER2
BLADE ATTACHMENT METHOD FIR TREE
OVERALL LENGTH2.440 INCHES MINIMUM AND 2.490 INCHES MAXIMUM
CRITICALITY CODE JUSTIFICATIONAGAV
END ITEM IDENTIFICATIONACFT TF39