1560-00-041-9979 CLEVIS,ROD END Index 1560-00-041-9992 MOUNT,COMPASS,MAGNETIC

National Stock Number:
5340-00-041-9980

Federal Supply Class:
5340

National Item Identification Number:
000419980

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:
S4382935-1218355THE BOEING COMPANY
S4382935-1288277THE BOEING COMPANY
S43829535-1200624EATON AEROQUIP LLC
S43829535-1231339MCGILL AIRCRAFT PARTS, INC.


Techincal Specification:
DISTANCE FROM PIVOT PINHOLE CENTER TO ROD CONNECTION END1.875 INCHES NOMINAL
END RADIUS0.250 INCHES NOMINAL
FORK ARM THICKNESS0.085 INCHES NOMINAL
FORK DEPTH0.990 INCHES MINIMUM AND 1.010 INCHES MAXIMUM
FORK SPAN WIDTH0.141 INCHES NOMINAL
HOLE DIAMETER0.187 INCHES MINIMUM AND 0.189 INCHES MAXIMUM
OVERALL WIDTH0.312 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONFED STD 66 FED STD SINGLE MATERIAL RESPONSE OR AISI/SAE ASSN STD SINGLE MATERIAL RESPONSE OVERALL
MATERIALSTEEL COMP 1035 OVERALL
SHANK DIAMETER0.428 INCHES MINIMUM AND 0.430 INCHES MAXIMUM
STYLE DESIGNATORCLEVIS
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONQQ-P-416,TYPE 2,CLASS 3 FED SPEC SINGLE TREATMENT RESPONSE OVERALL
SURFACE TREATMENTCADMIUM OVERALL
TEST DATA DOCUMENT81349-MIL-I-6868 SPECIFICATION (INCLUDES ENGINEERING TYPE BULLETINS, BROCHURES,ETC., THAT REFLECT SPECIFICATION TYPE DATA IN SPECIFICATION FORMAT; EXCLUDES COMMERCIAL CATALOGS, INDUSTRY DIRECTORIES, AND SIMILAR TRADE PUBLICATIONS, REFLECTING GENERAL TYPE DATA ON CERTAIN ENVIRONMENTAL AND PERFORMANCE REQUIREMENTS AND TEST CONDITIONS THAT ARE SHOWN AS "TYPICAL", "AVERAGE", "NOMINAL", ETC.).


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