1650-00-369-6514 CAMSHAFT,FEEDBACK,R Index 6685-00-369-6523 THERMOMETER,RECORDING,RESISTANCE

National Stock Number:
1680-00-369-6516

Federal Supply Class:
1680

National Item Identification Number:
003696516

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:
120-33994-194697MOOG INC
120-33994-19P5N5MOOG MILITARY AIRCRAFT LLC


Techincal Specification:
CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES1.495 INCHES MINIMUM AND 1.505 INCHES MAXIMUM
DISTANCE BETWEEN FORK INSIDE SPREAD0.237 INCHES MINIMUM AND 0.242 INCHES MAXIMUM
LINK END THICKNESS0.537 INCHES MINIMUM AND 0.542 INCHES MAXIMUM
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-A-225/9 FED SPEC 1ST MATERIAL RESPONSE OR QQ-A-250/12 FED SPEC 2ND MATERIAL RESPONSE
MATERIALALUMINUM ALLOY
SHAFT END THICKNESS0.495 INCHES MINIMUM AND 0.505 INCHES MAXIMUM
SPECIAL FEATURESTAP FOR 0.164-32 UNC 3B HELICAL COIL THROUGH END; OFFSET HEIGHT: 0.178 IN. MINIMUM AND 0.188 IN. MAXIMUM
STYLE DESIGNATORCLEVIS LINK END, SECURING HOLE(S) SHAFT END
SURFACE TREATMENTANODIZE


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