Part Number
Definition:
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.
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 |
---|---|---|
ASBP | BORE TYPE | SERRATED |
BFHN | DISTANCE BETWEEN FORK INSIDE SPREAD | 0.437 INCHES MINIMUM AND 0.442 INCHES MAXIMUM |
ABMK | OVERALL WIDTH | 0.562 INCHES NOMINAL |
AGJR | MINOR DIAMETER | 0.325 INCHES MINIMUM AND 0.328 INCHES MAXIMUM |
AAZR | MAJOR DIAMETER | 0.387 INCHES MINIMUM AND 0.390 INCHES MAXIMUM |
BFGW | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 2.750 INCHES NOMINAL |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/9, COMP 7075, T6 FED SPEC SINGLE MATERIAL RESPONSE |
MATT | MATERIAL | ALUMINUM ALLOY |
CZLP | SHAFT SECURING METHOD | SERRATIONS |
BFGY | LINK END THICKNESS | 0.625 INCHES NOMINAL |
ABSA | SPLINE QUANTITY | 11 |
BFGX | SHAFT END THICKNESS | 0.470 INCHES NOMINAL |
BFHA | LINK END HOLE DIAMETER | 0.190 INCHES NOMINAL |