Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-317-8324 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: 1319M30P01, 2840-01-317-8324, 01-317-8324, 2840013178324, 013178324
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 06, 1990 | 01-317-8324 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-317-8324
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1319M30P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-317-8324
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 3 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 6.774 INCHES MINIMUM AND 6.784 INCHES MAXIMUM |
| OVERALL WIDTH | 3.620 INCHES MINIMUM AND 3.640 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J79-15/17 AIRCRAFT ENGINE |