Product Details | AIRCRAFT GAS TURBINE ENGIN TURBINE NOZZLE ASSEMBLY

2840-01-441-0109 A stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle.

Part Alternates: 4083403, 2840-01-441-0109, 01-441-0109, 2840014410109, 014410109

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

Supply Group (FSG) NSN Assign. NIIN
28 01-441-0109

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Technical Data | NSN 2840-01-441-0109

Characteristic Specifications
DESIGN TYPE AXIAL COMPRESSOR
ENGINE SECTION LOCATION TURBINE
STAGE NUMBER 3
SPECIAL FEATURES ASSEMBLY IS MADE UP OF 23 P/N 4083213; 7 P/N 4083033 AND 1 P/N 4083023
CRITICALITY CODE JUSTIFICATION CZBJ AND CZCJ AND FEAT
III END ITEM IDENTIFICATION F100-PW-229 AIRCRAFT GAS TURBINE ENGINE
III PART NAME ASSIGNED BY CONTROLLING AGENCY ORIGINAL NAME TURBINE STATOR
MANUFACTURERS CODE 77445
DESIGN CONTROL REFERENCE 4083403

Restrictions/Controls & Freight Information | NSN 2840-01-441-0109

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