Part Details | AIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB
2840-01-207-0041 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: 4060942, 2840-01-207-0041, 01-207-0041, 2840012070041, 012070041
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | APR 26, 1985 | 01-207-0041 | 50573 ( HUB, COMPRESSOR, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-207-0041
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 4060942 | 77445 | UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS |
Technical Data | NSN 2840-01-207-0041
| Characteristic | Specifications |
|---|---|
| ENGINE SECTION LOCATION | COMPRESSOR |
| OVERALL LENGTH | 4.004 INCHES MINIMUM AND 4.014 INCHES MAXIMUM |
| SPECIAL FEATURES | THIS NSN IS AN F100 FRACTURE CRITICAL PART |
| END ITEM IDENTIFICATION | ACFT ENG F100-PW-220 |