Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-908-6981 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: 506871CL5, 315731CL5, 2840-00-908-6981, 00-908-6981, 2840009086981, 009086981
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1960 | 00-908-6981 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-908-6981
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 506871CL5 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 315731CL5 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-908-6981
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 3.985 INCHES MINIMUM AND 3.995 INCHES MAXIMUM |
| OVERALL WIDTH | 2.178 INCHES MINIMUM AND 2.204 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.763 INCHES MINIMUM AND 0.769 INCHES MAXIMUM |
| SPECIAL FEATURES | WAS VANE,TURBINE NOZZLE,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ENGINE MODEL J57 |