Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE ASSEMBLY
2840-01-192-0886 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: 4064083, 2840-01-192-0886, 01-192-0886, 2840011920886, 011920886
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 16, 1984 | 01-192-0886 | 50607 ( VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-192-0886
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4064083 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-192-0886
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | DIFFUSER |
| DIAMETER | 19.022 INCHES MINIMUM AND 19.028 INCHES MAXIMUM |
| REFERENCE DATA AND LITERATURE | T.O.2J-F100-24,FIGURE 137 |
| END ITEM IDENTIFICATION | F100-PW-220 TURBOFAN GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | COMPRESSOR 13 STAGE STATOR-EXIT VANE ASSEMBLY |