Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-444-8998 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: 1881M89G02, 1881M89, 2840-01-444-8998, 01-444-8998, 2840014448998, 014448998
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 19, 1997 | 01-444-8998 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-444-8998
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1881M89G02 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
| 1881M89 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-444-8998
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 1.873 INCHES MINIMUM AND 1.893 INCHES MAXIMUM |
| OVERALL WIDTH | 3.110 INCHES MINIMUM AND 3.130 INCHES MAXIMUM |
| SPECIAL FEATURES | ORIGINAL DRAWING NAME, NOZZLE,HIGH PRESSURE TURBINE-STAGE 1 MACHINING HT90-B,THIS IS PART OF THE HT90 MOD. FOR THE TF39 ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF39 |