NSN 2840-00-711-5742
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR VANE
2840-00-711-5742 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: 37E501067P101, 634E608P20, 37E501067P101, 634E608P20, 2840-00-711-5742, 00-711-5742, 2840007115742, 007115742
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-711-5742 | 50611 ( VANE, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-711-5742
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 37E501067P101 | 24446 | GENERAL ELECTRIC COMPANY |
| 634E608P20 | 24446 | GENERAL ELECTRIC COMPANY |
| 37E501067P101 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
| 634E608P20 | 99207 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-00-711-5742
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| STAGE NUMBER | 88 |
| BLADE ATTACHMENT METHOD | SLOT |
| OVERALL LENGTH | 4.061 INCHES MINIMUM AND 4.065 INCHES MAXIMUM |
| OVERALL WIDTH | 1.260 INCHES MINIMUM AND 1.275 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.0193 INCHES MINIMUM AND 0.0207 INCHES MAXIMUM |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | VANE,TURBINE ENGINE |