Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-122-1885 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: 6894587, 6865417, 6894587, 6894587, 2840-01-122-1885, 01-122-1885, 2840011221885, 011221885
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | NOV 15, 1981 | 01-122-1885 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-122-1885
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6894587 | 73342 | ALLISON TRANSMISSION, INC. |
| 6865417 | 73342 | ALLISON TRANSMISSION, INC. |
| 6894587 | 26199 | JOHNSON TECHNOLOGY, INC. |
| 6894587 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-01-122-1885
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| OVERALL LENGTH | 2.020 INCHES MINIMUM AND 2.030 INCHES MAXIMUM |
| DIAMETER | 26.348 INCHES NOMINAL |
| SPECIAL FEATURES | WAS VANE,TURBINE NOZZLE,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF41 |