Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE
2840-01-008-4442 A component of a VANE ASSEMBLY, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to receive air from the preceding compressor blades and deliver it to the succeeding row of compressor blades, diffuser, or combustion area at correct pressure, velocity and direction.
Alternate Parts: 765583, 748683, 2840-01-008-4442, 01-008-4442, 2840010084442, 010084442
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 24, 1975 | 01-008-4442 | 50611 ( VANE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-008-4442
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 765583 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 748683 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-008-4442
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 13 |
| OVERALL LENGTH | 2.230 INCHES MINIMUM AND 2.232 INCHES MAXIMUM |
| DIAMETER | 27.720 INCHES MINIMUM AND 27.740 INCHES MAXIMUM |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4, FIG17, IND25 |
| END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | COMPRESSOR STATOR 13 STAGE,ASST OF |