Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE ASSEMBLY
2840-01-114-4609 A stationary item designed for the purpose of directing air at the proper angle and velocity from a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud. The assembled item forms a complete circle.
Alternate Parts: 4063883, 4057183, 2840-01-114-4609, 01-114-4609, 2840011144609, 011144609
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUN 17, 1981 | 01-114-4609 | 50607 ( VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-114-4609
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4063883 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4057183 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-114-4609
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | DIFFUSER |
| DIAMETER | 19.073 INCHES NOMINAL |
| REFERENCE DATA AND LITERATURE | T.O.2J-F100-24,FIGURE 137 AGAVGF100-PW-220 TURBOFAN GAS TURBINE ENGINE |
| END ITEM IDENTIFICATION | U/O ACFT ENG F100 |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | COMPRESSOR 13TH STAGE STATOR-EXIT VANE ASSEMBLY |