Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE ASSEMBLY
2840-01-309-1200 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.
Alternate Parts: 407792003, 4077920-03, 2840-01-309-1200, 01-309-1200, 2840013091200, 013091200
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 11, 1989 | 01-309-1200 | 50581 ( NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-309-1200
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4077920-03 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-309-1200
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 10 |
| OVERALL LENGTH | 6.712 INCHES MINIMUM AND 6.716 INCHES MAXIMUM |
| SPECIAL FEATURES | INCLUDES 12TH STAGE AS WELL |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100-PW-229 AIRCRAFT ENGINE |