NSN 2840-01-444-6990 1881M31G02, 01-444-6990, 014446990
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 | Item Name Code (INC) |
---|---|---|---|
28 | 01-444-6990 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
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Related Products | NSN 2840-01-444-6990
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 Code | N | There 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 |