2995-01-057-2588 CONTROL ASSEMBLY,PUSH-PULL Index 5820-01-057-2591 MIXER,CRYSTAL,COAXIAL

National Stock Number:
3040-01-057-2590

Federal Supply Class:
3040

National Item Identification Number:
010572590

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:
53G97060176301THE BOEING COMPANY
53G970601-154T683AERO TECHNOLOGY COMPANY
53G970601-1576301THE BOEING COMPANY
53G970601-1588277THE BOEING COMPANY
53G970601-376301THE BOEING COMPANY
CS3040-SR-070216236DLA LAND AND MARITIME DBA ENGINEERING AND TECHNICAL SUPPORT DIV DOCUMENT STANDARDIZATION DIVISION (VENDOR ITEM DRAWINGS)
G970601-1576301THE BOEING COMPANY


Techincal Specification:
BODY CONSTRUCTIONSOLID
BODY THICKNESS0.322 INCHES MINIMUM AND 0.332 INCHES MAXIMUM
BODY WIDTH0.920 INCHES NOMINAL
CRITICALITY CODE JUSTIFICATIONFEAT
LINK STYLESTRAIGHT
OVERALL LENGTH2.200 INCHES NOMINAL
MATERIALALUMINUM ALLOY
SPECIAL FEATURESNEXT HIGHER ASSEMBLY - OUTER WING SLAT MECHANISM CONSISTS OF 53G9706C1-11, LINK AND MS14103-4 BEARING
SURFACE TREATMENTANODIZE


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