Product Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR DISK

2840-00-859-6804 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.

Part Alternates: 406203, 410703, 2840-00-859-6804, 00-859-6804, 2840008596804, 008596804

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

Supply Group (FSG) NSN Assign. NIIN
28 00-859-6804

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Technical Data | NSN 2840-00-859-6804

Characteristic Specifications
MATERIAL TITANIUM ALLOY OVERALL
MATERIAL DOCUMENT AND CLASSIFICATION AMS 4928 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
DESIGN TYPE AXIAL COMPRESSOR
ENGINE SECTION LOCATION COMPRESSOR
DIAMETER 10.740 INCHES NOMINAL
SPECIAL FEATURES DO NOT USE CADMIUM PLATED TOOLS ON THIS MATERIAL; WAS DISK,AXIAL COMPRESSOR,TURBINE ENGINE
CRITICALITY CODE JUSTIFICATION FEAT
III END ITEM IDENTIFICATION ACFT ENG. J-60
MANUFACTURERS CODE 77445
DESIGN CONTROL REFERENCE 410703

Restrictions/Controls & Freight Information | NSN 2840-00-859-6804

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