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 |
|---|---|
| 0JRC1 | NORTHROP GRUMMAN TECHNICAL SERVICES |
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 |
|---|---|---|
| CBBL | FEATURES PROVIDED | SPLIT END SCREW CLAMPING FEATURE |
| ASBP | BORE TYPE | SPLINED |
| FEAT | SPECIAL FEATURES | THIS ITEM HAS BEEN DETERMINED TO BE A CRITICAL APPLICATION ITEM. IN-FLIGHT FAILURE OF THIS ITEM WOULD CREATE A HAZARDOUS CONDITION |
| ABXV | BORE DIAMETER | 1.0625 INCHES MINIMUM AND 1.0640 INCHES MAXIMUM |
| BFGW | CENTER TO CENTER DISTANCE BETWEEN LINK AND SHAFT HOLES | 2.600 INCHES NOMINAL |
| BFHA | LINK END HOLE DIAMETER | 0.435 INCHES NOMINAL |
| ABSA | SPLINE QUANTITY | 5 |
| BFGY | LINK END THICKNESS | 1.055 INCHES NOMINAL |
| BFHN | DISTANCE BETWEEN FORK INSIDE SPREAD | 0.505 INCHES NOMINAL |
| AGAV | END ITEM IDENTIFICATION | T-38 AIRCRAFT |
| CRTL | CRITICALITY CODE JUSTIFICATION | FEAT |