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National Stock Number: 5340-00-176-0617
Federal Supply Class: 5340
National Item Identification Number: 001760617
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:
204-011-178-005 | 97499 | BELL TEXTRON INC | 204-011-178-5 | 54878 | ROTAIR AEROSPACE CORP | 204-011-178-5 | 97499 | BELL TEXTRON INC |
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Techincal Specification:
DISTANCE FROM CENTER OF SECURING PIN HOLE TO ROD END | 0.850 INCHES MINIMUM AND 0.910 INCHES MAXIMUM | HOLE DIAMETER | 0.505 INCHES MINIMUM AND 0.515 INCHES MAXIMUM | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-S-6758,COND F4 MIL SPEC SINGLE MATERIAL RESPONSE OVERALL | MATERIAL | STEEL COMP 4130 OVERALL | SPECIAL FEATURES | ADDITIONAL SECURING PIN HOLE DIAMETER 0.248 IN. MIN. 0.249 MAX.,0.510 IN. MIN. 0.515 MAX.; DISTANCE FROM CENTER OF SECURING PINHOLE TO END OF ROD,1.115 IN. MIN.,1.140 IN. MAX.,0.490IN. MIN. 0.515 IN. MAX. | SECURING PIN HOLE DIAMETER | 0.085 INCHES MINIMUM AND 0.088 INCHES MAXIMUM | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | 299-099-031,CB2,BELL HELICOPTER CO MFR REF SINGLE TREATMENT RESPONSE OVERALL | SURFACE TREATMENT | CADMIUM OVERALL |
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