Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB
2840-00-980-2669 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: 727617, 727617, 470571, 727617, 2840-00-980-2669, 00-980-2669, 2840009802669, 009802669
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-980-2669 | 50573 ( HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-980-2669
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 727617 | 50748 | BOGUE EXECUTIVE ENTERPRISES INCDBA/DEXTER TOOL CO |
| 727617 | 50381 | MTU AERO ENGINE COMPONENTS INC |
| 470571 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
| 727617 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-00-980-2669
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 14.533 INCHES MINIMUM AND 14.569 INCHES MAXIMUM |
| SPECIAL FEATURES | ORIGINAL NAME HUB,COMPRESSOR ROTOR,TURBINE ENGINE |
| CRITICALITY CODE JUSTIFICATION | AGAV |
| END ITEM IDENTIFICATION | TF-33 AIRCRAFT ENGINE |