3040-00-711-3507 BALL JOINT Index 2810-00-711-3517 SEAT,HELICAL COMPRESSION SPRING

National Stock Number:
5325-00-711-3511

Federal Supply Class:
5325

National Item Identification Number:
007113511

Description:
STUD ASSEMBLY,TURNLOCK FASTENER

Detail:
A STUD, TURNLOCK FASTENER over which may be assembled an EYELET, TURNLOCK FASTENER. Stud(s) without cam slots or cam lead threads are provided with a crosspin or eared nut for locking with the mating RECEPTACLE, TURNLOCK FASTENER. May be spring loaded. For like items having a threaded fastener, see SCREW ASSEMBLY, PANEL or SCREW, PANEL FASTENER.


Manufacturer Information:
2600-4SW71286HOWMET GLOBAL FASTENING SYSTEMS INC
2600-4SWD0680FAIRCHILD FASTENERS EUROPE CAMLOC GMBH
4188-2D9182ZF INDUSTRIEANTRIEBE WITTEN GMBH
55133-004F5442AIRBUS GROUP SAS
917473518876U S ARMY AVIATION AND MISSILE COMMAND
NSA55133-004F0210AIRBUS HELICOPTERS (ETS DEMARIGNANE)
NSA55133-004F5442AIRBUS GROUP SAS
S10036-4-405395L3HARRIS TECHNOLOGIES INTEGRATED SYSTEMS L.P.


Techincal Specification:
DISTANCE FROM ENGAGING MEMBER TO LARGEST BEARING SURFACE OF HEAD0.632 INCHES MINIMUM AND 0.647 INCHES MAXIMUM
EYELET LENGTH0.322 INCHES NOMINAL
EYELET OUTSIDE DIAMETER0.244 INCHES MINIMUM AND 0.250 INCHES MAXIMUM
HEAD LENGTH0.700 INCHES MINIMUM AND 0.740 INCHES MAXIMUM
MATERIAL ACCOMMODATED THICKNESS0.120 INCHES MINIMUM AND 0.149 INCHES MAXIMUM
MATERIALSTEEL OVERALL
STUD ASSEMBLY STYLESTUD ASSEMBLY
STUD HEAD HEIGHT0.448 INCHES MINIMUM AND 0.498 INCHES MAXIMUM
SURFACE TREATMENTPASSIVATE OVERALL
TURNLOCK STUD HEAD STYLEFILLISTER WING


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