|
|
National Stock Number: 5340-00-078-5595
Federal Supply Class: 5340
National Item Identification Number: 000785595
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.
|
Manufacturer Information:
3-93729-2 | 81205 | THE BOEING COMPANY |
|
Techincal Specification:
DISTANCE FROM PIVOT PINHOLE CENTER TO ROD CONNECTION END | 2.660 INCHES NOMINAL | END RADIUS | 0.125 INCHES NOMINAL | FORK ARM THICKNESS | 0.070 INCHES MINIMUM AND 0.090 INCHES MAXIMUM | FORK DEPTH | 1.380 INCHES NOMINAL | FORK SPAN WIDTH | 0.310 INCHES MINIMUM AND 0.315 INCHES MAXIMUM | HOLE DIAMETER | 0.250 INCHES MINIMUM AND 0.254 INCHES MAXIMUM | OVERALL DIAMETER | 0.750 INCHES NOMINAL | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-5000 MIL SPEC SINGLE MATERIAL RESPONSE OVERALL | MATERIAL | STEEL COMP 4340 OVERALL | SHANK DIAMETER | 0.380 INCHES MINIMUM AND 0.405 INCHES MAXIMUM | SHANK LENGTH | 1.160 INCHES NOMINAL | STYLE DESIGNATOR | CLEVIS | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | F-11923,THE BOEING CO MFR REF SINGLE TREATMENT RESPONSE OVERALL | SURFACE TREATMENT | CADMIUM OVERALL |
|
|