NSN 2840-00-759-6322
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE
2840-00-759-6322 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: 704272, 511472, 730782, 2840-00-759-6322, 00-759-6322, 2840007596322, 007596322
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1960 | 00-759-6322 | 50611 ( VANE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-759-6322
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 704272 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 511472 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 730782 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-759-6322
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 12 |
| OVERALL LENGTH | 2.400 INCHES MINIMUM AND 2.422 INCHES MAXIMUM |
| DIAMETER | 27.755 INCHES MINIMUM AND 27.765 INCHES MAXIMUM |
| SPECIAL FEATURES | 19.320-19.330 IN. ID |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | T.O. 2J-TF33-4 FIG17, IND18 |
| END ITEM IDENTIFICATION | TF33 AIRCRAFT ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | COMPRESSOR STATOR HALF,12 STAGE,ASSY OF |