Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB
2840-01-144-2473 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: 9084M40P01, 2840-01-144-2473, 01-144-2473, 2840011442473, 011442473
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | DEC 16, 1982 | 01-144-2473 | 50573 ( HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-144-2473
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 9084M40P01 | 07482 | GENERAL ELECTRIC COMPANYDBA GE |
Technical Data | NSN 2840-01-144-2473
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 1.100 INCHES MINIMUM AND 1.140 INCHES MAXIMUM |
| OVERALL WIDTH | 0.860 INCHES MINIMUM AND 0.920 INCHES MAXIMUM |
| MATERIAL THICKNESS | 0.185 INCHES NOMINAL |
| SPECIAL FEATURES | ORIG NAME HUB,COMPRESSOR FRAME |
| CRITICALITY CODE JUSTIFICATION | AAPGF$$ACZBJ$$AABHP$$AABMK$$AABPX |
| END ITEM IDENTIFICATION | ACFT ENG TF-39 |