Product Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB

2840-00-891-1883 A component of a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to attach to the front and/or rear of the rotor providing support, alignment, and a means of attachment for a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have provisions for installing bearings, and/or oil and air seals. See also DISK AND HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.

Part Alternates: 544487, 762666, 2840-00-891-1883, 00-891-1883, 2840008911883, 008911883

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

Supply Group (FSG) NSN Assign. NIIN
28 13 JAN 1967 00-891-1883

Cross Reference | NSN 2840-00-891-1883

Part Number Cage Code Manufacturer
544487 77445 UNITED TECHNOLOGIES CORPORATION DBA PRATT WHITNEY-SPARE PARTS
762666 77445 UNITED TECHNOLOGIES CORPORATION DBA PRATT WHITNEY-SPARE PARTS

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Technical Data | NSN 2840-00-891-1883

Characteristic Specifications
ENGINE SECTION LOCATION LOW PRESSURE COMPRESSOR
CRITICALITY CODE JUSTIFICATION AGAV
STAGE NUMBER 9
DESIGN TYPE COMPRESSOR
SPECIAL FEATURES T.O. 2J-J57-54; FRONT COMPRESSOR REAR
END ITEM IDENTIFICATION J57 AIRCRAFT ENGINE

Restrictions/Controls & Freight Information | NSN 2840-00-891-1883

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
Demilitarization Code:ANon-Munitions List Item/ Non-Strategic List Item - Demilitarization not required.
Precious Metals Indicator Code:AItem does not contain precious metal
Criticality Code:YThe item does not have a nuclear hardened feature but does have other critical feature(s) such as tolerance, fit restriction or application.
Category Code Description
No Freight Information