Product Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR BLADE

2840-00-533-5412 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: 2840-00-533-5412, 00-533-5412, 2840005335412, 005335412

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

Supply Group (FSG) NSN Assign. NIIN
28 00-533-5412

Cross Reference | NSN 2840-00-533-5412

Part Number Cage Code Manufacturer
254511 77445 UNITED TECHNOLOGIES CORPORATION DBA PRATT WHITNEY-SPARE PARTS
364911 52661 UNITED TECHNOLOGIES CORPORATION DBA PRATT & WHITNEY
364911 65115 TURBINE ENGINE COMPONENTS TEXTRON
364911 77445 UNITED TECHNOLOGIES CORPORATION DBA PRATT WHITNEY-SPARE PARTS

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Technical Data | NSN 2840-00-533-5412

Characteristic Specifications
DESIGN TYPE COMPRESSOR
ENGINE SECTION LOCATION COMPRESSOR
STAGE NUMBER 11
BLADE ATTACHMENT METHOD LOCK
SPECIAL FEATURES ORIGINAL NAME BLADE,COMRPESSOR ROTOR,TURBINE ENGINE
CRITICALITY CODE JUSTIFICATION AGAV
III END ITEM IDENTIFICATION J57 AIRCRAFT ENGINE
MANUFACTURERS CODE 77445
DESIGN CONTROL REFERENCE 254511

Restrictions/Controls & Freight Information | NSN 2840-00-533-5412

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