Part Details | ROD END BALL BEARING
3110-00-173-5074 A special single or multiple-row ball bearing, rigid or self-aligning, and constructed with either a solid or hollow shank, internally or externally threaded.
Alternate Parts: AN951RE3FL4MILG3, AN951RE3FL4, RE3FL4, 712016, L20885982, L2088598-2, AN951RE3FL4MILG3278, 502093, MS211534G, MS21153-4G, MS211534G, MS21153-4G, ABRL3F4G(L), ABRL3F-4G(L), MS211534G, MS21153-4G, REP3FL44G, REP3FL4-4G, 502093, RE3FL4MILG3278, MS211534G, MS21153-4G, AS6039, AS21153, RE3FL4MILG3278A, RE3FL4FS160, RE3FL4ANG25, RE3FL4, RE2FL4FS160A, REP3FL4FS464, CVC700RE3FL4, 3110-00-173-5074, 00-173-5074, 3110001735074, 001735074
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 31 | JAN 01, 1963 | 00-173-5074 | 00049 ( BEARING, BALL, ROD END ) |
REFERENCE DRAWINGS & PICTURES
INTERNALLY THREADED W/BEAD
DOUBLE ROW, STAGGERED, BALL
Cross Reference | NSN 3110-00-173-5074
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| AN951RE3FL4MILG3 | 88044 | AERONAUTICAL STANDARDS GROUPDEPT OF NAVY AND AIR FORCE |
| AN951RE3FL4 | 88044 | AERONAUTICAL STANDARDS GROUPDEPT OF NAVY AND AIR FORCE |
| RE3FL4 | 70413 | ANTI-FRICTION BEARING MFGASSN INC THE |
| 712016 | 21450 | ARMY WEAPONS COMMANDATTN AMSWE-REE-S |
| L2088598-2 | 94931 | BENDIX CORP THE BENDIX INTERNATIONALDIV |
| AN951RE3FL4MILG3278 | 80059 | JOINT AIRCRAFT COMMITTEE |
| 502093 | 02978 | L3 TECHNOLOGIES, INC.DBA COMBAT PROPULSION SYSTEMS |
| MS21153-4G | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
| MS21153-4G | 15860 | NEW HAMPSHIRE BALL BEARINGS, INC.DBA ASTRO DIVISION |
| ABRL3F-4G(L) | 15860 | NEW HAMPSHIRE BALL BEARINGS, INC.DBA ASTRO DIVISION |
| MS21153-4G | 73134 | ROLLER BEARING COMPANY OF AMERICA,INC. |
| REP3FL4-4G | 73134 | ROLLER BEARING COMPANY OF AMERICA,INC. |
| 502093 | R1120 | SATAIR A/S |
| RE3FL4MILG3278 | 38443 | SKF USA INC.DBA SKF AEROENGINE NORTH AMERICA |
| MS21153-4G | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS6039 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| AS21153 | 81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
| RE3FL4MILG3278A | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| RE3FL4FS160 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| RE3FL4ANG25 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| RE3FL4 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| RE2FL4FS160A | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| REP3FL4FS464 | 21335 | TIMKEN COMPANY, THEDIV TIMKEN AEROSPACE |
| CVC700RE3FL4 | 80378 | TRIUMPH AEROSTRUCTURES, LLCDBA TRIUMPH AEROSTRUCTURES - VOUGHT |
Technical Data | NSN 3110-00-173-5074
| Characteristic | Specifications |
|---|---|
| STYLE DESIGNATOR | DOUBLE ROW, STAGGERED, BALL |
| SELF-ALIGNMENT ANGLE | 10.00 DEGREES NOMINAL |
| OVERALL LENGTH | 1.7660 INCHES NOMINAL |
| BORE DIAMETER | 0.1900 INCHES NOMINAL |
| OVERALL OUTSIDE DIAMETER | 0.7810 INCHES NOMINAL |
| OUTER RING WIDTH | 0.3380 INCHES NOMINAL |
| INNER RING WIDTH | 0.5000 INCHES NOMINAL |
| LENGTH FROM BORE CENTER TO SHANK END | 1.3750 INCHES NOMINAL |
| SHANK STYLE | INTERNALLY THREADED W/BEAD |
| SHANK DIAMETER | 0.3750 INCHES NOMINAL |
| WIDTH ACROSS FLATS | 0.4380 INCHES NOMINAL |
| SHANK THREAD LENGTH | 0.7500 INCHES NOMINAL |
| THREAD SERIES DESIGNATOR | UNF |
| NOMINAL THREAD SIZE | 0.250 INCHES |
| THREAD QUANTITY PER INCH | 28 |
| THREAD CLASS | 3B |
| THREAD DIRECTION | LEFT-HAND |
| LUBRICATION MATERIAL | GREASE |
| LUBRICATION MATERIAL DOCUMENT AND CLASSIFICATION | MIL-G-23827 MIL SPEC SINGLE MATERIAL RESPONSE |
| SHIELD QUANTITY | 2 |
| ALIGNMENT TYPE | SELF-ALIGNING |
| SELF-ALIGNMENT LOCATION | INTERNAL |