Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-703-6862 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: 385851CL12, 2840-00-703-6862, 00-703-6862, 2840007036862, 007036862
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-703-6862 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-703-6862
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 385851CL12 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-703-6862
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | SLOT |
| SPECIAL FEATURES | T.O. 2J-J57-54; NOZZLE ASSY; INCLUDES STAGES 2-3; 1.311-1.320 SQ. IN. |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J57 AIRCRAFT ENGINE |