1560-00-035-4160 FITTING ASSEMBLY,ENGINE TRUNNION Index 1560-00-035-4166 CAM,MAIN ALIGHTING

National Stock Number:
1680-00-035-4165

Federal Supply Class:
1680

National Item Identification Number:
000354165

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:
192-3326143999THE BOEING COMPANY


Techincal Specification:
BORE DIAMETER0.242 INCHES NOMINAL
BORE LENGTH0.375 INCHES NOMINAL
BORE TYPEPLAIN STRAIGHT
CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES0.875 INCHES NOMINAL
DISTANCE BETWEEN FORK INSIDE SPREAD0.140 INCHES MINIMUM AND 0.145 INCHES MAXIMUM
LINK END HOLE DIAMETER0.188 INCHES NOMINAL
LINK END THICKNESS0.375 INCHES NOMINAL
OVERALL WIDTH0.438 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-225/6, 2024-T42 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALALUMINUM ALLOY
SHAFT END THICKNESS0.375 INCHES NOMINAL


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