1650-00-859-8711 ROD,PISTON,LINEAR ACTUATING CYLI Index 6615-00-859-8716 SHAFT ASSEMBLY

National Stock Number:
1680-00-859-8712

Federal Supply Class:
1680

National Item Identification Number:
008598712

Description:
LEVER,REMOTE CONTROL

Detail:
A rigid item usually in the form of an arm of various shapes and cross sections, containing two or more holes so spaced that one serves as a pivot with or without hubs and must have a definite means for securing to a shaft (such as threaded hole for set-screw, keyway(s), splines, serrations or some clamping device). The other hole(s) connect(s) to CONNECTING LINK, RIGID; WIRE ROPE ASSEMBLY, SINGLE LEG; or CLEVIS, ROD END; to provide transmission of movement to other parts of the mechanism. See also BELL CRANK. For manually operated items see LEVER, MANUAL CONTROL.


Manufacturer Information:
32-35060-576301THE BOEING COMPANY
32-35060-776301THE BOEING COMPANY


Techincal Specification:
BORE DIAMETER1.0620 INCHES MINIMUM AND 1.0635 INCHES MAXIMUM
BORE LENGTH2.410 INCHES NOMINAL
BORE TYPEPLAIN STRAIGHT
CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES3.000 INCHES NOMINAL
DISTANCE BETWEEN FORK INSIDE SPREAD0.343 INCHES MINIMUM AND 0.348 INCHES MAXIMUM
LINK END HOLE DIAMETER0.2495 INCHES MINIMUM AND 0.2505 INCHES MAXIMUM
LINK END THICKNESS0.643 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-367, COMP 7075, T6 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY
SHAFT END THICKNESS2.410 INCHES NOMINAL
SPECIAL FEATURESOFFSET HEIGHT: 0.883 IN. NOMINAL
STYLE DESIGNATORCLEVIS LINK END, SECURING HOLE(S) SHAFT END


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