3120-01-505-1162 BEARING,SLEEVE Index 5360-01-505-1164 SPRING,HELICAL,TORSION

National Stock Number:
3040-01-505-1163

Federal Supply Class:
3040

National Item Identification Number:
015051163

Description:
CONNECTING LINK,RIGID

Detail:
An item of various cross-sectional shapes which may be of solid or hollow construction. It is specifically designed for attachment to a lever(s) and/or control(s) to actuate various remote mechanisms. It is one of the following: (1) A one-piece item with or without eyes and/or holes in each end which may have bushings or bearings pressed in the eyes; (2) A one-piece item with both ends processed for terminations, excluding threaded end(s); (3) A two-piece construction type item consisting of a body with both ends processed for terminations and a single end attachment; or (4) A three-piece construction type item consisting of a body and two end attachments. Excludes internal combustion engine type piston connecting rods; DRAG LINK, STEERING; LINK, ANCHOR, BRAKE SHOE; TIE ROD, STEERING; and TURNBUCKLE. For cylindrical shaped externally threaded items without end attachments, see ROD, THREADED END and STUD (as modified).


Manufacturer Information:
69-1093817765THE BOEING COMPANY
69-1093881205THE BOEING COMPANY


Techincal Specification:
PART NAME ASSIGNED BY CONTROLLING AGENCYROD - THROTTLE AND START JT3D-1 ENGINE
PROPRIETARY CHARACTERISTICSPACS
SPECIAL FEATURESMATT 4130 STL TUBE; STOCK SIZE 1/2 O.D.X.083 OR .095 WALL;HEAT TREATED;ENDS TAP DRILL TO DEPTH .90 THREAD 3/8-24 UNF 2 B PER MIL-S-7742 EXC MAX MINOR DIA. SHALL BE .3400; CHAMFER 45 DEG. TO MAX THREAD DIA.; 1ST. END HAS .07 DIA HOLE THRU .38 IN AND CENTER FROM END; 2ND. END HAS 1/8 RIVET HOLE .30 IN AND CENTER FROM END
BODY CONSTRUCTIONTUBULAR
LINK STYLERETAINING PIN HOLE TO INTERNAL THREAD
MATERIAL DOCUMENT AND CLASSIFICATIONMIL-T-6736,NORMALIZED MIL SPEC SINGLE MATERIAL RESPONSE
MATERIALSTEEL


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