Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-122-1883 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: 4055823, 4055823, 2840-01-122-1883, 01-122-1883, 2840011221883, 011221883
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 15, 1981 | 01-122-1883 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-122-1883
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4055823 | 11449 | TURBO POWER & MARINE SYSTEM INCSUB OF UNITED TECHNOLOGIES CORP |
| 4055823 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-122-1883
| Characteristic | Specifications |
|---|---|
| DIAMETER | 2.500 INCHES NOMINAL |
| CRITICALITY CODE JUSTIFICATION | AABMZ$$AAGAV |
| END ITEM IDENTIFICATION | ACFT ENG F100 |