Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-308-3671 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: 4079942, 4079192, 4072682, 2840-01-308-3671, 01-308-3671, 2840013083671, 013083671
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 27, 1989 | 01-308-3671 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-308-3671
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4079942 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4079192 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4072682 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-308-3671
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 2 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 3.371 INCHES NOMINAL |
| OVERALL WIDTH | 1.830 INCHES MINIMUM AND 1.840 INCHES MAXIMUM |
| MATERIAL THICKNESS | 19.646 INCHES MINIMUM AND 19.766 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 AIRCRAFT ENGINE CORE |