Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-125-2212 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: 715853, 2840-01-125-2212, 01-125-2212, 2840011252212, 011252212
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 24, 1982 | 01-125-2212 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-125-2212
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 715853 | 03104 | TELEDYNE TECHNOLOGIES INCORPORATEDDBA TELEDYNE TURBINE ENGINES |
Technical Data | NSN 2840-01-125-2212
| Characteristic | Specifications |
|---|---|
| DIAMETER | 15.580 INCHES MINIMUM AND 15.586 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AMATT$$AABMZ$$AAGAV |
| END ITEM IDENTIFICATION | ACFT ENG J69 |