Product Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE

2840-01-388-8325 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.

Part Alternates: 2840-01-388-8325, 01-388-8325, 2840013888325, 013888325

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

Supply Group (FSG) NSN Assign. NIIN
28 01-388-8325

Cross Reference | NSN 2840-01-388-8325

Part Number Cage Code Manufacturer
P122P06 07482 GENERAL ELECTRIC COMPANY DBA GE

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Technical Data | NSN 2840-01-388-8325

Characteristic Specifications
MATERIAL TITANIUM ALLOY BLADE
DESIGN TYPE COMPRESSOR
ENGINE SECTION LOCATION COMPRESSOR
STAGE NUMBER 2
BLADE ATTACHMENT METHOD LOCK
OVERALL WIDTH 1.362 INCHES MAXIMUM
SPECIAL FEATURES PACER SPECIAL
CRITICALITY CODE JUSTIFICATION AGAV
III END ITEM IDENTIFICATION F118
MANUFACTURERS CODE 07482
DESIGN CONTROL REFERENCE P122P03

Restrictions/Controls & Freight Information | NSN 2840-01-388-8325

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