NSN 5325-01-502-6069

Part Details | RETAINING RING

5325-01-502-6069 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: 9M187C237, 9M187C237, 9M187C237, 9M187C237, 5325-01-502-6069, 01-502-6069, 5325015026069, 015026069

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
53NOV 14, 200201-502-606907623 ( RING, RETAINING )
REFERENCE DRAWINGS & PICTURES

ROUND

SPIRAL

Cross Reference | NSN 5325-01-502-6069
Part Number Cage Code Manufacturer
9M187C23776301BOEING COMPANY, THEDBA BOEING
9M187C23712837SEALTITE CORPORATION
9M187C23751814SMALLEY STEEL RING CO.
9M187C23780756SPIROLOX, INC.
Technical Data | NSN 5325-01-502-6069
Characteristic Specifications
MATERIAL STEEL CORROSION RESISTING
STRENGTH RATINGVAB221000.0 POUNDS PER SQUARE INCH
CASEHARDENING INDICATOR NOT CASEHARDENED
RING STYLE SPIRAL
CROSS-SECTIONAL SHAPE STYLE2 ROUND
USAGE DESIGN EXTERNAL
SURFACE TREATMENT PASSIVATE
INSIDE DIAMETER2.223 INCHES MINIMUM AND 2.248 INCHES MAXIMUM
OUTSIDE DIAMETER2.350 INCHES MINIMUM AND 2.375 INCHES MAXIMUM
MAJOR THICKNESS0.075 INCHES MINIMUM AND 0.081 INCHES MAXIMUM
CRITICALITY CODE JUSTIFICATIONAGAV
END ITEM IDENTIFICATIONF/A-18 AIRCRAFT
PART NAME ASSIGNED BY CONTROLLING AGENCY(INAVY) RING, RETAINING - EXTERNAL, SPIROLOX