National Stock Number (NSN) Output Data
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.
Reference/Part Number
| Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
|---|---|---|---|---|---|---|---|---|
| 507933 | 73030 | A | 3 | 2 | 2 | SB | ||
| 748849-1 | 73030 | A | C | 1 | 5 | ZZ | AC |
CAGE Information
| Code | Company |
|---|---|
| 73030 | HAMILTON SUNDSTRAND CORPORATION |
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 | 0.200 INCHES MINIMUM AND 0.210 INCHES MAXIMUM |
| AGJR | MINOR DIAMETER | 0.230 INCHES MINIMUM AND 0.232 INCHES MAXIMUM |
| BFGX | SHAFT END THICKNESS | 0.330 INCHES MINIMUM AND 0.340 INCHES MAXIMUM |
| ADDW | SERRATION QUANTITY | 18 |
| STYL | STYLE DESIGNATOR | CLEVIS LINK END, SECURING HOLE(S) SHAFT END |
| BFGW | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 0.640 INCHES NOMINAL |
| MATT | MATERIAL | STEEL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AHS 256, A4 H1075, UNITED TECHNOLOGIES CORP ASSN STD 5TH MATERIAL RESPONSE |
| BFGY | LINK END THICKNESS | 0.330 INCHES MINIMUM AND 0.340 INCHES MAXIMUM |
| CZLP | SHAFT SECURING METHOD | SERRATIONS |
| AAZR | MAJOR DIAMETER | 0.255 INCHES MINIMUM AND 0.257 INCHES MAXIMUM |