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National Stock Number:
5340-00-788-6621
Federal Supply Class:
5340
National Item Identification Number:
007886621
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:
| 32-61020-3 | 76301 | THE BOEING COMPANY |
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Techincal Specification:
| DISTANCE FROM PIVOT PINHOLE CENTER TO ROD CONNECTION END | 2.440 INCHES NOMINAL | | FORK ARM THICKNESS | 0.100 INCHES NOMINAL | | FORK DEPTH | 1.120 INCHES NOMINAL | | FORK SPAN WIDTH | 0.242 INCHES NOMINAL | | HOLE DIAMETER | 0.2495 INCHES MINIMUM AND 0.2505 INCHES MAXIMUM | | OVERALL WIDTH | 0.422 INCHES NOMINAL | | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/6,T4 FED SPEC SINGLE MATERIAL RESPONSE OVERALL | | MATERIAL | ALUMINUM ALLOY 2024 OVERALL | | ROD CONNECTION BORE DEPTH | 1.000 INCHES NOMINAL | | ROD CONNECTION BORE DIAMETER | 0.500 INCHES NOMINAL | | SHANK DIAMETER | 0.866 INCHES MINIMUM AND 0.870 INCHES MAXIMUM | | SHANK LENGTH | 1.220 INCHES NOMINAL | | STYLE DESIGNATOR | CLEVIS | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | TT-L-32 FED SPEC SINGLE TREATMENT RESPONSE BODY | | SURFACE TREATMENT | LACQUER BODY |
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