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National Stock Number:
5340-00-906-2194
Federal Supply Class:
5340
National Item Identification Number:
009062194
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:
| S6126-50104-1 | 78286 | SIKORSKY AIRCRAFT CORPORATION |
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Techincal Specification:
| DISTANCE FROM PIVOT PINHOLE CENTER TO ROD CONNECTION END | 8.120 INCHES NOMINAL | | END RADIUS | 1.125 INCHES NOMINAL | | FORK SPAN WIDTH | 0.895 INCHES MINIMUM AND 0.896 INCHES MAXIMUM | | FORK ARM THICKNESS | 0.300 INCHES NOMINAL | | FORK DEPTH | 1.500 INCHES NOMINAL | | HOLE DIAMETER | 0.749 INCHES MINIMUM AND 0.750 INCHES MAXIMUM | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/9 FED SPEC SINGLE MATERIAL RESPONSE BODY | | MATERIAL | ALUMINUM ALLOY 7075 BODY | | OVERALL DIAMETER | 3.181 INCHES MINIMUM AND 3.183 INCHES MAXIMUM | | ROD CONNECTION BORE DEPTH | 4.120 INCHES NOMINAL | | ROD CONNECTION BORE DIAMETER | 2.875 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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