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National Stock Number:
5340-01-510-9120
Federal Supply Class:
5340
National Item Identification Number:
015109120
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:
| 17P1N6173-1 | 88277 | THE BOEING COMPANY |
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Techincal Specification:
| FORK ARM THICKNESS | 0.099 INCHES MINIMUM AND 0.129 INCHES MAXIMUM | | FORK DEPTH | 0.290 INCHES MINIMUM AND 0.320 INCHES MAXIMUM | | FORK SPAN WIDTH | 0.205 INCHES MINIMUM AND 0.215 INCHES MAXIMUM | | III MATERIAL | ALUMINUM ALLOY 705.0 OVERALL | | PROPRIETARY CHARACTERISTICS | PACS | | OVERALL WIDTH | 0.433 INCHES MINIMUM AND 0.443 INCHES MAXIMUM | | SPECIAL FEATURES | MANUFACTURERS NOMENCLATURE IS CLEVIS, ROD END, WIPER MOTOR, WINDSHIELD;CONNECTOR ROD HAS HOLES 0.190 IN.DIA. TO0.192 IN. DIA.;DISTANCE BETWEEN ROD END CENTER HOLE AND FORK HOLE CENTER IS 0.535 IN. POM 0.015 IN;DISTANCE BETWEEN FORK EDGE AND ROD END HOLE CENTER IS0.219IN. POM 0.015 | | STYLE DESIGNATOR | CLEVIS | | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL | | SURFACE TREATMENT | ANODIZE OVERALL |
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