NSN 5340-01-193-7108

Part Details | ROD END CLEVIS

5340-01-193-7108 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.

Alternate Parts: L5803193003, L5803193-003, 5340-01-193-7108, 01-193-7108, 5340011937108, 011937108

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
53NOV 07, 198401-193-710803796 ( CLEVIS, ROD END )
REFERENCE DRAWINGS & PICTURES

CLEVIS

Cross Reference | NSN 5340-01-193-7108
Part Number Cage Code Manufacturer
L5803193-00343999BOEING COMPANY, THEDBA BOEING
Technical Data | NSN 5340-01-193-7108
Characteristic Specifications
STYLE DESIGNATOR3 CLEVIS
END RADIUS0.250 INCHES NOMINAL
OVERALL DIAMETER0.500 INCHES NOMINAL
FORK SPAN WIDTH0.125 INCHES MINIMUM AND 0.130 INCHES MAXIMUM
DISTANCE FROM PIVOT PINHOLE CENTER TO ROD CONNECTION END0.750 INCHES NOMINAL
FORK ARM THICKNESS0.093 INCHES NOMINAL
FORK DEPTH0.312 INCHES NOMINAL
HOLE DIAMETER0.2500 INCHES MINIMUM AND 0.2522 INCHES MAXIMUM
SPECIAL FEATURES0.070 IN. DIA HOLE THROUGH SHANK 30.0 DEG FROM CLEVIS END,CENTER 0.093 IN. FROM END AND 0.219 IN. FROM SIDE; FLATS ON SIDE PARALELL TO CLEVIS TO 0.438 IN. ACROSS FLATS