Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-445-4013 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: 4082943CLP, 4082943, 2840-01-445-4013, 01-445-4013, 2840014454013, 014454013
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 02, 1997 | 01-445-4013 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-445-4013
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4082943CLP | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4082943 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-445-4013
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 2.246 INCHES MINIMUM AND 2.254 INCHES MAXIMUM |
| OVERALL WIDTH | 2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM |
| OVERALL HEIGHT | 4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 132, FLOW AREA 4.664-4.689 |
| CRITICALITY CODE JUSTIFICATION | AABMK$$AABHP$$AABKW$$AFEAT$$ACZCJ |
| END ITEM IDENTIFICATION | F100-PW-100 AIRCRAFT GAS TURBINE ENGINE |