5945-01-004-4350 RELAY,REED Index 3040-01-004-4352 CONNECTING LINK,RIGID

National Stock Number:
3040-01-004-4351

Federal Supply Class:
3040

National Item Identification Number:
010044351

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:
160C122002-161174NORTHROP GRUMMAN SYSTEMS CORPORATION
160C122002-179RG9NORTHROP GRUMMAN SYSTEMS CORPORATION
3500-134742TYEE AIRCRAFT INC
3535-134742TYEE AIRCRAFT INC
SR11011S97393SPS TECHNOLOGIES LLC


Techincal Specification:
END ATTACHMENT STYLEEYE FIRST END
BODY CONSTRUCTIONTUBULAR
BODY THICKNESS0.661 INCHES NOMINAL
LINK STYLESOLID SHANK
OVERALL LENGTH3.251 INCHES MINIMUM AND 3.523 INCHES MAXIMUM
PART NAME ASSIGNED BY CONTROLLING AGENCYPUSHROD - CLASS A, TYPE I, VERTICAL DRIVE, FS 267, ROLL CONTROL
SPECIAL FEATURESMAXIMUM ALLOWABLE WEIGHT: .25LBS; OPERATING LOADS: 0LB TO 54LB TENSION; 0LB TO 54LB COMPRESSION;STATIC LOADS: DESIGN LIMIT LOAD = 440LBS TENSION AND 440LBS COMPRESSION; DESIGN ULTIMATE LOAD: 660LBS TENSION AND 660LBS COMPRESSION; PROOF LOAD TEST: 1000LBS COMPRESSION; 1000LBS TENSION (FOLLOWING COMPRESSION TEST); INK STAMP "PL" AFTER SUCCESSFUL COMPLETION OF BOTH TESTS


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