Product Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE

2840-01-107-6232 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: 2840-01-107-6232, 01-107-6232, 2840011076232, 011076232

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

Supply Group (FSG) NSN Assign. NIIN
28 01-107-6232

Cross Reference | NSN 2840-01-107-6232

Part Number Cage Code Manufacturer
6021T21P13 99207 GENERAL ELECTRIC COMPANY DBA GE

Request a Quote

What Our Customers Say

Compare

NSNs for Compare ( up to 4 ): Add 2840-01-107-6232

Technical Data | NSN 2840-01-107-6232

Characteristic Specifications
MATERIAL STEEL BLADE
DESIGN TYPE COMPRESSOR
ENGINE SECTION LOCATION HIGH PRESSURE COMPRESSOR
STAGE NUMBER 11
OVERALL LENGTH 0.885 INCHES NOMINAL
OVERALL WIDTH 0.395 INCHES NOMINAL
SPECIAL FEATURES ORIGINAL NAME BLADE,COMPRESSOR ROTOR,TURBINE ENGINE
CRITICALITY CODE JUSTIFICATION AGAV
III END ITEM IDENTIFICATION ACFT ENG TF34
MANUFACTURERS CODE 99207
DESIGN CONTROL REFERENCE 6021T21P09

Restrictions/Controls & Freight Information | NSN 2840-01-107-6232

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