Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE SEGMENT
2840-01-234-0848 A portion of a NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It consists of two or more NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE cast as one piece.
Alternate Parts: 4070251CLL, 4070251, 2840-01-234-0848, 01-234-0848, 2840012340848, 012340848
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 06, 1986 | 01-234-0848 | 50583 ( NOZZLE SEGMENT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-234-0848
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4070251CLL | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4070251 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-234-0848
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 1 |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 155, IND 32; 1.730-1.749 SQ. IN .AREA; 1800 CYCLE; TURBINE STATOR SUPPORT; REID/REPLACED P/NS 4045851CLN, 4056781CLL AND 4059181CL1 |
| CRITICALITY CODE JUSTIFICATION | FEAT |
| END ITEM IDENTIFICATION | ACFT.ENG. F100/200 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME NOZZLE ASSEMBLY, TURBINE, AIRCRAFT GAS TURBINE ENGINE |