Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB
2840-00-018-4073 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: 698999, 466009, 822636, 2840-00-018-4073, 00-018-4073, 2840000184073, 000184073
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-018-4073 | 50573 ( HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-018-4073
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 698999 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 466009 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 822636 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-018-4073
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 16.485 INCHES MINIMUM AND 16.505 INCHES MAXIMUM |
| DIAMETER | 18.802 INCHES MINIMUM AND 18.804 INCHES MAXIMUM |
| SPECIAL FEATURES | 2ND END DIA. 5.495-5.500; 3 HOLES 0.120-0.130 IN. DIA.; 16 HOLES 0.437-0.439 IN. DIA.; 16 HOLES 0.374-0.376 IN. DIA. |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | ACFT ENG TF33 |