1560-00-767-9568 FLAP HINGE,AILERON Index 1560-00-767-9571 SHAFT,IDLER CRANK

National Stock Number:
1680-00-767-9570

Federal Supply Class:
1680

National Item Identification Number:
007679570

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:
2-13813-10JRC1NORTHROP GRUMMAN TECHNICAL SERVICES, INC.
2-13813-11TM86INTERNATIONAL AERO ENGINEERING, LLC
2-13813-11ZKE3MILITARY AIRCRAFT PARTS
2-13813-132664AEROMETALS, INC.
2-13813-13Q1K2AERO DEFENSE CORPORATION
2-13813-13Z260A. J. ASSOCIATES MANUFACTURING & ENGINEERING CO. INC.
2-13813-14R2Y5A WILEY & ASSOCIATES INC
2-13813-1586P5SPIRIT AVIATION SERVICES INC.
2-13813-15H716PCA AEROSPACE, INC.
2-13813-15H860THOMAS INSTRUMENT, INCORPORATED
2-13813-15SEG9TEXAS MILITARY SUPPLY DBA CONSTRUCTION MATERIALS DIVISION DIV CONSTRUCTION MATERIALS DIVISION
2-13813-16M132SKYSPARES PARTS INC
2-13813-176823NORTHROP GRUMMAN SYSTEMS CORPORATION
2-13813-179U29NORTHROP GRUMMAN SYSTEMS CORPORATION


Techincal Specification:
BORE TYPESERRATED
CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES3.000 INCHES NOMINAL
LINK END THICKNESS0.710 INCHES MINIMUM AND 0.750 INCHES MAXIMUM
LINK END HOLE DIAMETER0.190 INCHES NOMINAL
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-M-55, AZ92A-T6 FED SPEC SINGLE MATERIAL RESPONSE
MATERIALMAGNESIUM ALLOY
SHAFT END THICKNESS0.750 INCHES NOMINAL
SHAFT SECURING METHODSPLINE


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