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)
53JAN 01, 196300-052-541407623 ( RING, RETAINING )
REFERENCE DRAWINGS & PICTURES

RECTANGULAR

RING,RETAINING | 5325-00-052-5414, 000525414

EXTERNAL INVERTED LUGS

RING,RETAINING | 5325-00-052-5414, 000525414
Cross Reference | NSN 5325-00-052-5414
Part Number Cage Code Manufacturer
A-632-S07400-00672166B.W. ELLIOTT MANUFACTURING CO., LLCDBA ELLIOTT MANUFACTURING
12109 ITEM 1172166B.W. ELLIOTT MANUFACTURING CO., LLCDBA ELLIOTT MANUFACTURING
A1636-776275CESSNA AIRCRAFT COMCCAULEY ACCESSORY DIV
MS16626-107596906MILITARY STANDARDSPROMULGATED BY MILITARY DEPARTMENTS
5108-75MD07382ROTOR CLIP COMPANY INC.DBA ROTOR CLAMP
4100-75-ST-CD07382ROTOR CLIP COMPANY INC.DBA ROTOR CLAMP
4100-75-ST-CD97464TRUARC CO LLC
5108-75MD79136TRUARC COMPANY LLCDBA WALDES TRUARC
5108-75-MFD9182ZF 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 RATING66.0 ROCKWELL SUPERFICIAL 30-N MINIMUM AND 71.0 ROCKWELL SUPERFICIAL 30-N MAXIMUM
SURFACE TREATMENT CADMIUM AND CHROMATE
INSIDE DIAMETER0.683 INCHES MINIMUM AND 0.698 INCHES MAXIMUM
MAJOR THICKNESS0.040 INCHES MINIMUM AND 0.044 INCHES MAXIMUM