Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE
2840-01-444-7672 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: 4083091, 4083091, 4083091, 4082991, 4069391, 2840-01-444-7672, 01-444-7672, 2840014447672, 014447672
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAY 15, 1997 | 01-444-7672 | 50611 ( VANE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-444-7672
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4083091 | 52661 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY |
| 4083091 | 0ZB13 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT & WHITNEY MILITARY |
| 4083091 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4082991 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 4069391 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-444-7672
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | AXIAL COMPRESSOR |
| ENGINE SECTION LOCATION | HIGH PRESSURE TURBINE |
| STAGE NUMBER | 1 |
| OVERALL LENGTH | 3.713 INCHES NOMINAL |
| SPECIAL FEATURES | ORIGINAL DRAWING NAME, VANE TURBINE STATOR 1 STAGE, ASSY OF |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG F100PW229 |
