NSN 3040-00-006-4516

Part Details | RIGID CONNECTING LINK


3040-00-006-4516 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).

Alternate Parts: A51B975081, A51B97508-1, A51B975081, A51B97508-1, A51B975085, A51B97508-5, A51B975083, A51B97508-3, A51B975081, A51B97508-1, A51B975085, A51B97508-5, A51B975081, A51B97508-1, 3040-00-006-4516, 00-006-4516, 3040000064516, 000064516

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
30JUN 25, 197200-006-451621988 ( CONNECTING LINK, RIGID )
REFERENCE DRAWINGS & PICTURES

90 DEG OFFSET HOLES


Cross Reference | NSN 3040-00-006-4516
Part Number Cage Code Manufacturer
A51B97508-10VSV7AIRCRAFT TUBULAR COMPONENTS, INC.
A51B97508-196547FLEET READINESS CENTER SOUTHEASTDIV NAVY
A51B97508-526512NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS
A51B97508-326512NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS
A51B97508-126512NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV MISSION SYSTEMS
A51B97508-561174NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE
A51B97508-161174NORTHROP GRUMMAN SYSTEMS CORPORATIONDIV NORTHROP GRUMMAN AEROSPACE

Technical Data | NSN 3040-00-006-4516
Characteristic Specifications
MATERIAL STEEL
BODY CONSTRUCTION SOLID
LINK STYLE 90 DEG OFFSET HOLES
OVERALL LENGTH2.161 INCHES MINIMUM AND 2.171 INCHES MAXIMUM
BODY WIDTH0.580 INCHES MINIMUM AND 0.585 INCHES MAXIMUM
BODY THICKNESS0.248 INCHES MINIMUM AND 0.250 INCHES MAXIMUM
SPECIAL FEATURESWEAPON SYSTEM ESSENTIAL
CRITICALITY CODE JUSTIFICATIONFEAT
END ITEM IDENTIFICATIONF-14 TOMCAT AIRCRAFT.