NSN 2840-00-243-7739
Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB
2840-00-243-7739 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: 569445, 2840-00-243-7739, 00-243-7739, 2840002437739, 002437739
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | MAR 10, 1971 | 00-243-7739 | 50573 ( HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-243-7739
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 569445 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-243-7739
| Characteristic | Specifications |
|---|---|
| DESIGN TYPE | COMPRESSOR |
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 18.710 INCHES NOMINAL |
| OVERALL HEIGHT | 6.415 INCHES NOMINAL |
| SPECIAL FEATURES | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| REFERENCE DATA AND LITERATURE | 2J-TF33-4 FIG 19 |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |
