Product Details | AIRCRAFT GAS TURBINE ENGIN TURBINE NOZZLE ASSEMBLY

2840-01-444-6990 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: 1881M31G02, 2840-01-444-6990, 01-444-6990, 2840014446990, 014446990

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

Supply Group (FSG) NSN Assign. NIIN
28 01-444-6990

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Technical Data | NSN 2840-01-444-6990

Characteristic Specifications
DESIGN TYPE AXIAL COMPRESSOR
ENGINE SECTION LOCATION HIGH PRESSURE TURBINE
STAGE NUMBER 1
SPECIAL FEATURES T.O. 2J-TF39-4, FIG 54, IND 162; REPL P/N 9687M93G53; BUT NOT TO BE GROUPED DUE TO TOTAL RECONFIGURATION OF ITEM PER ECP 369; DCN 97-37
CRITICALITY CODE JUSTIFICATION CZBJ AND FEAT
III END ITEM IDENTIFICATION TF-39 AIRCRAFT GAS TURBINE ENGINE
MANUFACTURERS CODE 07482
DESIGN CONTROL REFERENCE 1881M31G02

Restrictions/Controls & Freight Information | NSN 2840-01-444-6990

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