Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB
2840-00-439-1711 A component of a ROTOR, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE. It is designed to attach to the front and/or rear of the rotor providing support, alignment, and a means of attachment for a SHAFT, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have provisions for installing bearings, and/or oil and air seals. See also DISK AND HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 6701418, 6701418, 6701418, 2840-00-439-1711, 00-439-1711, 2840004391711, 004391711
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-439-1711 | 50573 ( HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-439-1711
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 6701418 | 73342 | ALLISON TRANSMISSION, INC. |
| 6701418 | 24617 | GENERAL MOTORS CORP |
| 6701418 | 63005 | ROLLS-ROYCE CORPORATION |
Technical Data | NSN 2840-00-439-1711
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | CENTRIFUGAL |
| ENGINE SECTION LOCATION | COMPRESSOR |
| CRITICALITY CODE JUSTIFICATION | CZBJ |
| END ITEM IDENTIFICATION | J-33 AIRCRAFT ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |