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		                        | 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).
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 Manufacturer Information:
 
 | 69-10938 | 17765 | THE BOEING COMPANY |  | 69-10938 | 81205 | THE BOEING COMPANY | 
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 Techincal Specification:
 
 | PART NAME ASSIGNED BY CONTROLLING AGENCY | ROD - THROTTLE AND START JT3D-1 ENGINE |  | PROPRIETARY CHARACTERISTICS | PACS |  | SPECIAL FEATURES | MATT 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 CONSTRUCTION | TUBULAR |  | LINK STYLE | RETAINING PIN HOLE TO INTERNAL THREAD |  | MATERIAL DOCUMENT AND CLASSIFICATION | MIL-T-6736,NORMALIZED MIL SPEC SINGLE MATERIAL RESPONSE |  | MATERIAL | STEEL | 
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