Part Details | ANNULAR BALL BEARING
3110-00-151-8104 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: GS03A1076G, GS03A107-6G, RS772D5579MILG3278A, RS77NR3H, 77NR3HZFIE, RS772D5579MILG3278A, RS77NR3H, A25A709034103, A25A709-034-103, 03771, 0377-1, NA03771, NA0377-1, A25A709034103, A25A709-034-103, 2021061001, 2021061-001, FB3FFMB1STA019Y75C00000, FB3FFMB1STA019Y75C0000-0, F3DD160A0, F3DDMILG3278A, F3DDMILG3278, F3DDFS25735, F3DDFS160L, F3DDFS160, F3DDE5116, F3DDC1MILG3278, F3DDC1FS160, SMB28707610, SMB287076-10, 3110-00-151-8104, 00-151-8104, 3110001518104, 001518104
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 31 | JAN 01, 1963 | 00-151-8104 | 00014 ( BEARING, BALL, ANNULAR ) |
REFERENCE DRAWINGS & PICTURES
NON-LOADING GROOVE, NON-SEPARABLE
Cross Reference | NSN 3110-00-151-8104
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| GS03A107-6G | 67116 | COMPUTRONICS INC |
| RS772D5579MILG3278A | 24617 | GENERAL MOTORS CORP |
| RS77NR3H | 24617 | GENERAL MOTORS CORP |
| 77NR3HZFIE | 43334 | GENERAL MOTORS CORPDELCO MORAINE NDH DIV |
| RS772D5579MILG3278A | 43334 | GENERAL MOTORS CORPDELCO MORAINE NDH DIV |
| RS77NR3H | 43334 | GENERAL MOTORS CORPDELCO MORAINE NDH DIV |
| A25A709-034-103 | 73842 | GOODYEAR TIRE AND RUBBER CO THE |
| 0377-1 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| NA0377-1 | 56232 | LOCKHEED MARTIN CORPORATIONDBA LOCKHEED MARTIN |
| A25A709-034-103 | 99696 | LOCKHEED MARTIN CORPORATIONDIV LOCKHEED MARTIN SYSTEMS & GLOBAL |
| 2021061-001 | 10001 | NAVAIR AND NAVSEA MANAGEDORIGINAL DESIGN ACTIVITY DWG NOT |
| FB3FFMB1STA019Y75C0000-0 | 38443 | SKF USA INC.DBA SKF AEROENGINE NORTH AMERICA |
| F3DD160A0 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| F3DDMILG3278A | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| F3DDMILG3278 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| F3DDFS25735 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| F3DDFS160L | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| F3DDFS160 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| F3DDE5116 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| F3DDC1MILG3278 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| F3DDC1FS160 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| SMB287076-10 | 80063 | US ARMY COMMUNICATIONS &ELECTRONICS MATERIEL READINESS |
Technical Data | NSN 3110-00-151-8104
| Characteristic | Specifications |
|---|---|
| STYLE DESIGNATOR | NON-LOADING GROOVE, NON-SEPARABLE |
| OUTER RING TAPER | 0.0800 NOMINAL |
| BORE DIAMETER | 0.1875 INCHES MINIMUM AND 0.1878 INCHES MAXIMUM |
| FLANGE OUTSIDE DIAMETER | 0.6250 INCHES NOMINAL |
| FLANGE WIDTH | 0.0420 INCHES NOMINAL |
| OUTER RING WIDTH | 0.2260 INCHES NOMINAL |
| INNER RING WIDTH | 0.2490 INCHES MINIMUM AND 0.2510 INCHES MAXIMUM |
| LUBRICATION MATERIAL | GREASE |
| LUBRICATION MATERIAL DOCUMENT AND CLASSIFICATION | MIL-G-23827 MIL SPEC SINGLE MATERIAL RESPONSE |
| BORE SHAPE | STRAIGHT |
| SURFACE FINISH | GROUND |
| RETAINER FABRICATION METHOD | PRESSED |
| SHIELD QUANTITY | 2 |
| LOAD DIRECTION | RADIAL |
| INTERNAL FIT-UP DESIGNATION | STANDARD |
| SPECIAL FEATURES | BORE CORNER CHAMFERED 0.0100 IN. BY 45 DEG |