1650-00-981-8015 SHAFT ASSY,CYLINDER Index 1560-00-981-8023 PANEL ASSEMBLY,WING

National Stock Number:
3040-00-981-8019

Federal Supply Class:
3040

National Item Identification Number:
009818019

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:
69-10800-281205THE BOEING COMPANY


Techincal Specification:
DISTANCE BETWEEN FORK INSIDE SPREAD0.600 INCHES NOMINAL
BORE TYPESPLINED
CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES3.920 INCHES NOMINAL
LINK END HOLE DIAMETER0.250 INCHES NOMINAL
LINK END THICKNESS0.800 INCHES NOMINAL
MAJOR DIAMETER0.650 INCHES MINIMUM AND 0.658 INCHES MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATIONAMS 5362 ASSN STD SINGLE MATERIAL RESPONSE
III MATERIALSTEEL
PROPRIETARY CHARACTERISTICSPACS
MINOR DIAMETER0.5625 INCHES MINIMUM AND 0.5655 INCHES MAXIMUM
SHAFT END THICKNESS0.340 INCHES NOMINAL
SHAFT SECURING METHODSPLINE
SPECIAL FEATURESOFFSET HEIGHT: 0.230 IN. NOMINAL
SPLINE QUANTITY19
STYLE DESIGNATORCLEVIS LINK END, SECURING HOLE(S) SHAFT END


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