NSN 2840-00-909-5510
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-909-5510 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: 6853952, 6853952, 6853952, 2840-00-909-5510, 00-909-5510, 2840009095510, 009095510
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1960 | 00-909-5510 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-909-5510
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6853952 | 73342 | ALLISON TRANSMISSION, INC. |
| 6853952 | 24617 | GENERAL MOTORS CORP |
| 6853952 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-00-909-5510
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 1 |
| SPECIAL FEATURES | T.O. 2J-T56-44, FIG 20A, IND 10; USED ON POS 5, 10, 15, 20, 25 AND 30; WEU 6870728; WEU 6896898 U/W 6852237 OR 6856654; WEU 23031747 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | AIRCRAFT ENGINE MODEL T56 |