NSN 5325-00-052-5414
Part Details | RETAINING RING
5325-00-052-5414 A resilient metal item, circular or nearly circular, which is designed to be inserted into an internal or external groove and retained by its own spring action, or it may have external prongs or projections designed to be inserted into a hole and retained by spring action of the prongs which grip by imbedding into the material. For items having internal prongs which perform the same function, see PUSH ON NUT. It is used to keep and/or lock a part(s) in position, as a ball bearing on a shaft or in a housing. See also CLIP, RETAINING and PIN, LOCK. Excludes RING, CONNECTING, ROUND.
Alternate Parts: A632S07400006, A-632-S07400-006, 12109 ITEM 11, A16367, A1636-7, MS166261075, MS16626-1075, 510875MD, 5108-75MD, 410075STCD, 4100-75-ST-CD, 410075STCD, 4100-75-ST-CD, 510875MD, 5108-75MD, 510875MF, 5108-75-MF, 5325-00-052-5414, 00-052-5414, 5325000525414, 000525414
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
53 | JAN 01, 1963 | 00-052-5414 | 07623 ( RING, RETAINING ) |
REFERENCE DRAWINGS & PICTURES
RECTANGULAR
EXTERNAL INVERTED LUGS
Cross Reference | NSN 5325-00-052-5414
Part Number | Cage Code | Manufacturer |
---|---|---|
A-632-S07400-006 | 72166 | B.W. ELLIOTT MANUFACTURING CO., LLCDBA ELLIOTT MANUFACTURING |
12109 ITEM 11 | 72166 | B.W. ELLIOTT MANUFACTURING CO., LLCDBA ELLIOTT MANUFACTURING |
A1636-7 | 76275 | CESSNA AIRCRAFT COMCCAULEY ACCESSORY DIV |
MS16626-1075 | 96906 | MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS |
5108-75MD | 07382 | ROTOR CLIP COMPANY INC.DBA ROTOR CLAMP |
4100-75-ST-CD | 07382 | ROTOR CLIP COMPANY INC.DBA ROTOR CLAMP |
4100-75-ST-CD | 97464 | TRUARC CO LLC |
5108-75MD | 79136 | TRUARC COMPANY LLCDBA WALDES TRUARC |
5108-75-MF | D9182 | ZF INDUSTRIEANTRIEBE WITTEN GMBH |
Technical Data | NSN 5325-00-052-5414
Characteristic | Specifications |
---|---|
CASEHARDENING INDICATOR | NOT CASEHARDENED |
RING STYLE | EXTERNAL INVERTED LUGS |
CROSS-SECTIONAL SHAPE STYLE | RECTANGULAR |
USAGE DESIGN | EXTERNAL |
MATERIAL HARDNESS RATING | 66.0 ROCKWELL SUPERFICIAL 30-N MINIMUM AND 71.0 ROCKWELL SUPERFICIAL 30-N MAXIMUM |
SURFACE TREATMENT | CADMIUM AND CHROMATE |
INSIDE DIAMETER | 0.683 INCHES MINIMUM AND 0.698 INCHES MAXIMUM |
MAJOR THICKNESS | 0.040 INCHES MINIMUM AND 0.044 INCHES MAXIMUM |