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National Stock Number: 5340-00-017-3309
Federal Supply Class: 5340
National Item Identification Number: 000173309
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:
S6122-87265-3 | 78286 | SIKORSKY AIRCRAFT CORPORATION |
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Techincal Specification:
DISTANCE FROM PIVOT PINHOLE CENTER TO ROD CONNECTION END | 2.810 INCHES NOMINAL | END RADIUS | 0.500 INCHES NOMINAL | FORK ARM THICKNESS | 0.180 INCHES MINIMUM AND 0.190 INCHES MAXIMUM | FORK DEPTH | 0.750 INCHES NOMINAL | FORK SPAN WIDTH | 0.550 INCHES MINIMUM AND 0.560 INCHES MAXIMUM | HOLE DIAMETER | 0.2495 INCHES MINIMUM AND 0.2505 INCHES MAXIMUM | OVERALL HEIGHT | 1.000 INCHES NOMINAL | OVERALL WIDTH | 0.910 INCHES MINIMUM AND 0.940 INCHES MAXIMUM | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/9,T651 FED SPEC SINGLE MATERIAL RESPONSE BODY | MATERIAL | ALUMINUM ALLOY 7075 BODY | SHANK DIAMETER | 0.648 INCHES MINIMUM AND 0.650 INCHES MAXIMUM | SHANK LENGTH | 1.810 INCHES NOMINAL | STYLE DESIGNATOR | CLEVIS | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 MIL SPEC SINGLE TREATMENT RESPONSE BODY | SURFACE TREATMENT | ANODIZE BODY |
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