NSN 5325-00-527-1986

Part Details | RETAINING RING

5325-00-527-1986 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: 402047, 327B436P5, RD15951216, RD15951-216, RR216, RR-216, MCF13375, RR216, 6260019162, 626-001-9162, RR216, 105989161, 10598916-1, 10043943174, 10043943-174, 402047, 5325-00-527-1986, 00-527-1986, 5325005271986, 005271986

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
53JAN 01, 196300-527-198607623 ( RING, RETAINING )
REFERENCE DRAWINGS & PICTURES

ROUND

SPECIAL FLAT

Cross Reference | NSN 5325-00-527-1986
Part Number Cage Code Manufacturer
40204733823ADAMS INDUSTRIES INCA SUB OF BANNER INDUSTRIES INC
327B436P533823ADAMS INDUSTRIES INCA SUB OF BANNER INDUSTRIES INC
RD15951-21651663CRANE CO.DBA LEAR ROMEC
RR-21672547DETROIT BALL BEARING CO OF MICHIGAN
MCF1337576050EATON AEROSPACE LLCM C AEROSPACE DIV
RR21603350GENERAL ELECTRIC COMPANYDBA GE STRUCTURED SERVICES DIV
626-001-916270210HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
RR21680756SPIROLOX, INC.
10598916-118876U S ARMY AVIATION AND MISSILECOMMAND
10043943-17418876U S ARMY AVIATION AND MISSILECOMMAND
40204777445UNITED TECHNOLOGIES CORPORATIONDBA PRATT WHITNEY-SPARE PARTS
Technical Data | NSN 5325-00-527-1986
Characteristic Specifications
STRENGTH RATING211000.0 POUNDS PER SQUARE INCH MINIMUM TENSILE
CASEHARDENING INDICATOR NOT CASEHARDENED
RING STYLE SPECIAL FLAT
CROSS-SECTIONAL SHAPE STYLE2 ROUND
USAGE DESIGN INTERNAL
INSIDE DIAMETER1.984 INCHES NOMINAL
OUTSIDE DIAMETER2.260 INCHES NOMINAL
MAJOR THICKNESS0.048 INCHES NOMINAL
END ITEM IDENTIFICATIONW/S:GUIDED MISSILE, INTERCEPT; ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); HELICOPTER, SEA KNIG H-3; AIRCRAFT, F-111; ENGINE, AIRCRAFT, J85-GE-21 (F-5E/F); AIRCRAFT, THUNDERBOLT II, A-10; ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135. B-52H); HELICOPTER, MH-53E; ENGINE, AIRCRAFT, J85-GE-5/13 (F-5A/B, T-38A)