Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE SEGMENT
2840-01-234-0847 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: 4059951CLL, 4059951, 2840-01-234-0847, 01-234-0847, 2840012340847, 012340847
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 06, 1986 | 01-234-0847 | 50583 ( NOZZLE SEGMENT, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-234-0847
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4059951CLL | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4059951 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-234-0847
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 1 |
| SPECIAL FEATURES | T.O. 2J-F100-14, FIG 155, IND 30; 1800 CYCLE; 1.730-1.749 SQ. IN. AREA; TURBINE STATOR SUPPORT; REID/REPLACED P/NS 4045951CLL, 4056771CLL AND 4059191CLL |
| 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 |