NSN 3040-01-443-9799

Part Details | REMOTE CONTROL LEVER

3040-01-443-9799 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.

Alternate Parts: 1476AS2322, 1476AS232-2, 1476AS2322, 1476AS232-2, 1476AS2322, 1476AS232-2, 3040-01-443-9799, 01-443-9799, 3040014439799, 014439799

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
30APR 24, 199701-443-979922099 ( LEVER, REMOTE CONTROL )
REFERENCE DRAWINGS & PICTURES

FLAT, ONE HOLE LINK END

Cross Reference | NSN 3040-01-443-9799
Part Number Cage Code Manufacturer
1476AS232-230003NAVAL AIR SYSTEMS COMMAND MANAGEDORIGINAL DESIGN ACTIVITY NOT
1476AS232-228638NAVAL AIR WARFARE CENTER AIRCRAFTDIVISION CODE 1.3.1 BLDG 562-1
1476AS232-280020NAVAL AIR WARFARE CENTER AIRCRAFTDIVISION CODE 4.8.8.0.0.B BLDG 148-2
Technical Data | NSN 3040-01-443-9799
Characteristic Specifications
MATERIAL STEEL
MATERIAL DOCUMENT AND CLASSIFICATIONQQ-S-7863, CLASS 304 FED SPEC SINGLE MATERIAL RESPONSE
STYLE DESIGNATOR5 FLAT, ONE HOLE LINK END
CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES2.000 INCHES NOMINAL
LINK END THICKNESS0.450 INCHES NOMINAL
END ITEM IDENTIFICATIONT400-CP400 FOR H1 HELICOPTER
PART NAME ASSIGNED BY CONTROLLING AGENCYLEVER ENGINE CONTROL,TIE ROD ASSY TURBOSHAFT ENGINE TEST SYSTEM