1560-00-083-6006 FLAP,WING LANDING Index 5365-00-083-6016 SHIM

National Stock Number:
5340-00-083-6012

Federal Supply Class:
5340

National Item Identification Number:
000836012

Description:
CLEVIS,ROD END

Detail:
A forked part, having transverse hole(s) or slot(s) in each arm (prong) to accommodate a bolt, pin, or the like, and having a connection facility opposite the fork. It is designed to be attached to a shaft, rod, turnbuckle or the like by welding, threading, and/or pinning. May include provisions for locking. See also YOKE, UNIVERSAL JOINT and CONNECTOR, ROD END. For items specifically designed for aviation, see CLEVIS, ROD END, AVIATION.


Manufacturer Information:
5354-502121GOODRICH AEROSPACE CANADA LTD.


Techincal Specification:
DISTANCE FROM PIVOT PINHOLE CENTER TO ROD CONNECTION END1.156 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATIONAAUB
END RADIUS0.250 INCHES NOMINAL
FORK ARM THICKNESS0.133 INCHES NOMINAL
FORK DEPTH0.609 INCHES MINIMUM AND 0.619 INCHES MAXIMUM
FORK SPAN WIDTH0.484 INCHES MINIMUM AND 0.489 INCHES MAXIMUM
HOLE DIAMETER0.2495 INCHES MINIMUM AND 0.2500 INCHES MAXIMUM
OVERALL HEIGHT0.500 INCHES NOMINAL
OVERALL WIDTH0.750 INCHES MINIMUM AND 0.760 INCHES MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATIONMIL-S-5000,COND D MIL SPEC SINGLE MATERIAL RESPONSE OVERALL
MATERIALSTEEL COMP 4340 OVERALL
ROD CONNECTION BORE DEPTH0.547 INCHES NOMINAL
ROD CONNECTION BORE DIAMETER0.218 INCHES NOMINAL
SHANK DIAMETER0.562 INCHES NOMINAL
SHANK LENGTH0.312 INCHES NOMINAL
SPECIAL FEATURESSHANK END THD 0.562-24 NEF-3A,LG OF THD 0.212 IN.
STYLE DESIGNATORCLEVIS
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONQQ-P-416,TYPE 1B FED SPEC SINGLE TREATMENT RESPONSE OVERALL
SURFACE TREATMENTCADMIUM OVERALL


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