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National Stock Number: 5340-01-212-2386
Federal Supply Class: 5340
National Item Identification Number: 012122386
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.
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Manufacturer Information:
458-52229-5 | 81205 | THE BOEING COMPANY | 458-52229-5 | 82918 | THE BOEING COMPANY |
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Techincal Specification:
DISTANCE FROM PIVOT PINHOLE CENTER TO ROD CONNECTION END | 2.300 INCHES NOMINAL | DISTANCE FROM CENTER OF SECURING PIN HOLE TO ROD END | 0.640 INCHES NOMINAL | END RADIUS | 0.330 INCHES NOMINAL | FORK DEPTH | 0.760 INCHES NOMINAL | FORK SPAN WIDTH | 0.180 INCHES NOMINAL | FORK ARM THICKNESS | 0.090 INCHES NOMINAL | HOLE DIAMETER | 0.250 INCHES MINIMUM AND 0.261 INCHES MAXIMUM | OVERALL WIDTH | 0.360 INCHES NOMINAL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS 5659 ASSN STD SINGLE MATERIAL RESPONSE OVERALL | MATERIAL | STEEL COMP XM-12 OVERALL | SECURING PIN HOLE DIAMETER | 0.190 INCHES MINIMUM AND 0.199 INCHES MAXIMUM | SHANK DIAMETER | 0.430 INCHES NOMINAL | SHANK LENGTH | 1.400 INCHES NOMINAL | STYLE DESIGNATOR | CLEVIS | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | QQ-P-35 FED SPEC SINGLE TREATMENT RESPONSE OVERALL | SURFACE TREATMENT | PASSIVATE OVERALL |
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