NSN 2840-00-076-9779
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE
2840-00-076-9779 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: 702051CL5, 2840-00-076-9779, 00-076-9779, 2840000769779, 000769779
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 16, 1971 | 00-076-9779 | 50611 ( VANE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-076-9779
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 702051CL5 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-076-9779
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMBUSTION CHAMBER |
| STAGE NUMBER | 1 |
| BLADE ATTACHMENT METHOD | PIN |
| OVERALL LENGTH | 2.614 INCHES MINIMUM AND 2.663 INCHES MAXIMUM |
| OVERALL WIDTH | 1.104 INCHES MINIMUM AND 1.124 INCHES MAXIMUM |
| SPECIAL FEATURES | T.O. 2J-J60-4; 0.892-0.901 FLOW AREA; TURBINE NOZZLE,CASC,OULET DUCT;MADE OF COLBALT ALLOY |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | J60 AIRCRAFT ENGINE |