Part Number
Definition:
A CONTROL CONSISTING OF A WIRE, WIRE ROPE, OR A CENTER LOAD RAIL WITH BALL BEARINGS, WITHIN A FLEXIBLE CONDUIT. ONE END MUST HAVE A THREADED SLEEVE FOR MOUNTING TO A WALL, BULKHEAD, OR HANDLE, OR CLEVIS. IT IS USED TO OPERATE OR CONTROL, EITHER MANUALLY OR MECHANICALLY A MECHANICAL DEVICE. IT MAY INCLUDE SUCH ATTACHING DEVICES AS NUT(S), WASHER(S), CLEVIS, BRACKET(S), AND/OR THE LIKE. FOR ITEMS DESIGNED TO TRANSMIT ROTARY MOTION, SEE SHAFT ASSEMBLY, FLEXIBLE.
CAGE Information
Code | Company |
---|---|
43999 | BOEING COMPANY THE DBA BOEING DIV DE |
Federal Supply Class
Title
MISCELLANEOUS AIRCRAFT ACCESSORI
Inclusions:
INCLUDES CONTROL ASSEMBLIES, PUSH-PULL; BRACE, POSITIONING CARGO RAMP STOWED ON BOARD; COCKPIT MOUNTED CONTROL QUADRANTS; ACTUATORS, ELECTRO-MECHANICAL AND MECHANICAL; VENTILATORS; RELIEF TUBES; MAP HOLDERS; AERIAL GLIDER TOWING ACCESSORIES ATTACHED TO AIRCRAFT; BELTS, SAFETY AND LAP; HARNESS, SHOULDER AND SAFETY; LITTER ATTACHING SUPPORTS;ELECTRIC WINDSHIELD WIPERS;AIRCRAFT ONBOARD INERT GAS GENERATORS;AIRCRAFT FURNITURE;AIRCRAFT MOUNTED WINCHES AND HOISTS;IN-FLIGHT REFUELING SYSTEM COMPONENTS, INCLUDING FUEL COMPONENTS;AIRCRAFT CURTAINS;CABLE TENSION REGULATORS;SUN VISORS;REAR-VIEW MIRRORS;MECHANICAL TRANSMISSIONS, GEARBOXES AND CONSTANT SPEED DRIVES SPECIALLY DESIGNED FOR AIRCRAFT.
Exclusions:
EXCLUDES ENGINE MOUNTED CONTROL ASSEMBLIES; FITTED COVERS, AIRCRAFT PYLONS; HELICOPTER ROTER BRAKE SYSTEM COMPONENTS; HELICOPTER AUTOMATIC STABILIZATION EQUIPMENT.
Characteristics (Decoded)
MRC | Requirements Statement | Clear Text Reply |
---|---|---|
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | MANUFACTURERS SUGGESTED NAME - PULL ROD, INTERMEDIATE, UPPER - PRI FLT CONT ASSY |
BCYD | FLEXIBLE CONDUIT OUTSIDE DIAMETER | 0.187 INCHES NOMINAL |
ABNZ | EFFECTIVE LENGTH | 306.430 INCHES MINIMUM AND 306.490 INCHES MAXIMUM |
AFKT | FLEXIBLE CONDUIT MATERIAL | STEEL CORROSION RESISTING |
AGAV | END ITEM IDENTIFICATION | B-1B ACFT |