Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-444-6553 A single 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.
Alternate Parts: 1864M32G01, 1864M32, 2840-01-444-6553, 01-444-6553, 2840014446553, 014446553
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 13, 1997 | 01-444-6553 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-444-6553
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1864M32G01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1864M32 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-444-6553
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 2 |
| OVERALL LENGTH | 4.117 INCHES NOMINAL |
| SPECIAL FEATURES | DIFFERENT FROM 1864M32G02 NOTE LOCATION OF HOLES DRILLED ON STACKING AXIS OF AIRFOILS, ALSO NOTE THIS IS PART OF THE HT90 MOD FOR THE TF39 ENGINE, ALSO NOTE THE DRAWING NAME IS NOZZLE, HIGH PRESSURE TURBINE-STAGE 2 MACHINING, AND NOZZLE IS COATED WITH NICKEL PLATING, ALSO LENGTH IS 4.11745 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |