5315-01-495-1132 PIN,STRAIGHT,HEADLESS Index 5998-01-495-1134 ELECTRONIC COMPONENTS ASSEMBLY

National Stock Number:
5340-01-495-1133

Federal Supply Class:
5340

National Item Identification Number:
014951133

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:
17P2G1370-50588277THE BOEING COMPANY


Techincal Specification:
DISTANCE FROM PIVOT PINHOLE CENTER TO ROD CONNECTION END0.500 INCHES NOMINAL
FORK ARM THICKNESS0.078 NOMINAL INCHES
FORK SPAN WIDTH0.470 INCHES NOMINAL
HOLE DIAMETER0.060 INCHES NOMINAL
HOLE SHAPEROUND
MATERIAL DOCUMENT AND CLASSIFICATIONAMS5659 ASSN STD SINGLE MATERIAL RESPONSE OVERALL
III MATERIALSTEEL CORROSION RESISTING OVERALL
PROPRIETARY CHARACTERISTICSPACS
NOMINAL THREAD SIZE0.250 INCHES STUD END
OVERALL HEIGHT0.555 INCHES MINIMUM AND 0.565 INCHES MAXIMUM
OVERALL WIDTH0.626 INCHES NOMINAL
SHANK LENGTH0.800 INCHES NOMINAL
SPECIAL FEATURESORIGINAL DWG NAME=TARGET ASSY, ADS; OA LG 3.790 IN.; THERE ARE 2 COAXIAL HOLES W/O.D. OF 0.312-0.316, I.D. OF 0.0218-0.229 IN;2 OTHER HOLES W/DIA OF 0.193-0.196 IN., THE C TO C DIST BTWN THESE HOLES IS 0.699 IN.; DIST FROM CNTR OF COAXIAL HOLES TO ROD END IS 3.514 IN.
STYLE DESIGNATORCLEVIS
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONQQ-P-35 FED SPEC SINGLE TREATMENT RESPONSE OVERALL
SURFACE TREATMENTPASSIVATE OVERALL
THREAD CLASS3B STUD END
THREAD DIRECTIONRIGHT-HAND STUD END
THREAD LENGTH0.312 INCHES NOMINAL STUD END
THREAD QUANTITY PER INCH28 STUD END
THREAD SERIES DESIGNATORUNJF STUD END


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