Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE ASSEMBLY
2840-01-448-7512 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: 4084343CLN, 4084343, 2840-01-448-7512, 01-448-7512, 2840014487512, 014487512
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 09, 1997 | 01-448-7512 | 50607 ( VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-448-7512
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4084343CLN | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4084343 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-448-7512
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | TURBINE |
| STAGE NUMBER | 3 |
| OVERALL LENGTH | 4.717 INCHES MINIMUM AND 4.737 INCHES MAXIMUM |
| OVERALL WIDTH | 2.036 INCHES MINIMUM AND 2.084 INCHES MAXIMUM |
| DIAMETER | 13.410 INCHES MINIMUM AND 13.450 INCHES MAXIMUM |
| SPECIAL FEATURES | 4.639-4.664 SQUARE INCH FLOW AREA |
| CRITICALITY CODE JUSTIFICATION | ACZBJ$$AABHP$$AABMZ$$AABMK$$AFEAT |
| END ITEM IDENTIFICATION | F100-PW-220 AIRCRAFT GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME VANE,TURBINE STATORASSEMBLY |