NSN 3110-00-602-4231
Part Details | ANNULAR BALL BEARING
3110-00-602-4231 A cylindrical device in which the inner or outer ring turns upon a single or double row of hardened balls which roll easily between the two rings, thus minimizing friction. For items with faces specially ground for duplex mounting see BEARING, BALL, DUPLEX. Excludes BEARING, BALL, AIRFRAME.
Alternate Parts: 12203301, 122033-01, Z83, Z106K5VL430, 7920201, 79202-01, 79202, 12203301, 122033-01, 77SR3JTHZF5582J9, SR3DTHLR5292, RS77SR3JTHZF5582J9, SR3DTHLR5292, 4653871, 465387-1, 12203301, 122033-01, M33KDD53E7344, M33KDD5-3E7344, MV33KDD53E7344, MV33KDD5-3E7344, MM33K8FS25550, 3110-00-602-4231, 00-602-4231, 3110006024231, 006024231
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
31 | JAN 01, 1963 | 00-602-4231 | 00014 ( BEARING, BALL, ANNULAR ) |
REFERENCE DRAWINGS & PICTURES
NON-LOADING GROOVE, NON-SEPARABLE

Cross Reference | NSN 3110-00-602-4231
Part Number | Cage Code | Manufacturer |
---|---|---|
122033-01 | 70854 | BARDEN CORPORATION, THEDIV BARDEN PRECISION BEARINGS |
Z83 | 70854 | BARDEN CORPORATION, THEDIV BARDEN PRECISION BEARINGS |
Z106K5VL430 | 70854 | BARDEN CORPORATION, THEDIV BARDEN PRECISION BEARINGS |
79202-01 | 35351 | GE AVIATION SYSTEMS LLC |
79202 | 35351 | GE AVIATION SYSTEMS LLC |
122033-01 | 35351 | GE AVIATION SYSTEMS LLC |
77SR3JTHZF5582J9 | 24617 | GENERAL MOTORS CORP |
SR3DTHLR5292 | 24617 | GENERAL MOTORS CORP |
RS77SR3JTHZF5582J9 | 24617 | GENERAL MOTORS CORP |
SR3DTHLR5292 | 43334 | GENERAL MOTORS CORPDELCO MORAINE NDH DIV |
465387-1 | 96214 | RAYTHEON COMPANYDBA RAYTHEON |
122033-01 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
M33KDD5-3E7344 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
MV33KDD5-3E7344 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
MM33K8FS25550 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
Technical Data | NSN 3110-00-602-4231
Characteristic | Specifications |
---|---|
STYLE DESIGNATOR | NON-LOADING GROOVE, NON-SEPARABLE |
BORE DIAMETER | 0.1873 INCHES MINIMUM AND 0.1875 INCHES MAXIMUM |
OVERALL OUTSIDE DIAMETER | 0.6225 INCHES MINIMUM AND 0.6235 INCHES MAXIMUM |
OUTER RING WIDTH | 0.2120 INCHES NOMINAL |
INNER RING WIDTH | 0.2110 INCHES MINIMUM AND 0.2120 INCHES MAXIMUM |
LUBRICATION MATERIAL | OIL |
LUBRICATION MATERIAL DOCUMENT AND CLASSIFICATION | MIL-L-6085 MIL SPEC SINGLE MATERIAL RESPONSE |
BORE SHAPE | STRAIGHT |
SURFACE FINISH | GROUND |
RETAINER FABRICATION METHOD | COILED |
SHIELD QUANTITY | 2 |
LOAD DIRECTION | RADIAL |
INTERNAL CLEARANCE | R0.0005 INCHES MINIMUM AND R0.0008 INCHES MAXIMUM |
SPECIAL FEATURES | INNER RING RADIAL RUNOUT 0.0002 IN.; OUTER RING RADIAL RUNOUT 0.0004 IN.; STRATING TORQUE 0.3600 GM CM UNDER 400 GM THRUST LOAD; SLOTS EQUALLY SPACED CUT INTO FACE OF EXTENDED SIDE OF OUTER RING 0.6300 IN. W ON 0.5000 CUTTER R,CHORDAL LG NOT TO EXCEED 0.5720 IN.; OUTER RING OD THREADED 0.6250 IN. 40 NS; 0.0250 IN. TO 0.4000 IN. BY 45 DEG CHAMFER 0N OD CORNERS; 11BALLS 1 MM DIA 0.00001 SPHERICITY,0.00002 IN. MAX VARIATEION |