Product Details | AIRCRAFT GAS TURBINE ENGINE FAN BLADE

2840-01-472-6304 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.

Part Alternates: 2840-01-472-6304, 01-472-6304, 2840014726304, 014726304

Engines, Turbines, and Components | Gas Turbines and Jet Engines, Aircraft, Prime Moving; and Components

Supply Group (FSG) NSN Assign. NIIN
28 01-472-6304

Cross Reference | NSN 2840-01-472-6304

Part Number Cage Code Manufacturer
1993M18P03 07482 GENERAL ELECTRIC COMPANY DBA GE
1993M18P04 07482 GENERAL ELECTRIC COMPANY DBA GE

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Technical Data | NSN 2840-01-472-6304

Characteristic Specifications
MATERIAL TITANIUM OVERALL
DESIGN TYPE AXIAL COMPRESSOR
ENGINE SECTION LOCATION FAN
STAGE NUMBER 1
BLADE ATTACHMENT METHOD DOVETAIL
OVERALL LENGTH 13.000 INCHES NOMINAL
OVERALL WIDTH 3.750 INCHES NOMINAL
MATERIAL THICKNESS 0.500 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATION AGAV
REFERENCE DATA AND LITERATURE T.O. 2J-F101-4, FIG17, IND8
III END ITEM IDENTIFICATION F101GE102 ACFT ENG B-1B ACFT
III PART NAME ASSIGNED BY CONTROLLING AGENCY RUGGEDIZED STAGE 1 FAN BLADE
MANUFACTURERS CODE 07482
DESIGN CONTROL REFERENCE 1993M18P04

Restrictions/Controls & Freight Information | NSN 2840-01-472-6304

Category Code Description
Hazardous Material Indicator CodeNThere is no data in the HMIS and the NSN is in an FSC not generally suspected of containing hazardous materials
Category Code Description
No Freight Information