Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-318-4800 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: 4075534, 2840-01-318-4800, 01-318-4800, 2840013184800, 013184800
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 19, 1990 | 01-318-4800 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-318-4800
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4075534 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-318-4800
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 4 |
| BLADE ATTACHMENT METHOD | PIN |
| SPECIAL FEATURES | ADDT'L P/N 4068967,56 REQD; P/N 4075254,28 REQD; P/N 4074848,PIN,56 REQD; P/N 4061774,COLLAR,56 REQD; P/N 4068968 |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | F100PW0229 ENGINE/FDT MOD |