NSN 2835-00-340-7686
Part Details | NONAIRCRAFT GAS TURBINE ENGINE COMPRESSOR HUB
2835-00-340-7686 A component of a ROTOR, COMPRESSOR, NONAIRCRAFT 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, NONAIRCRAFT GAS TURBINE ENGINE. It may have provisions for installing bearings, and/or oil and air seals. See also DISK AND HUB, COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE.
Alternate Parts: 75974, 75974, 75974, 2835-00-340-7686, 00-340-7686, 2835003407686, 003407686
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JAN 01, 1963 | 00-340-7686 | 50574 ( HUB, COMPRESSOR, NONAIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2835-00-340-7686
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 75974 | 72599 | ALLIEDSIGNAL INCDBA ALLIED-SIGNAL AEROSPACE CO |
| 75974 | 70210 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
| 75974 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2835-00-340-7686
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | MATERIAL STEEL ROD,4130,MIL-S-6758,SHOULDER DIA 0.840 IN. MIN TO 0.870 IN. MAX,1ST END OD 0.560 IN.,1ST END LG 0.685 IN.,1ST END ID CHAMFER 0.010 IN. BY 43.0 TO 47.0 DEG,2ND END OD 0.6260 IN.,2ND END LG 0.678 IN.,2ND END ID CHAMFER 0.020 IN. BY 43.0 TO 47.0 DEG,O/A ID OF HUB 0.4670 IN. |
| END ITEM IDENTIFICATION | 61157585492 |
| FSC APPLICATION DATA | POWER UNIT,GAS TURBINE ENGINE |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | HUB,COMPRESSOR ROTOR,TURBINE ENGINE |