NIIN 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 |
---|---|---|---|---|---|---|---|---|
L5247110-007 | 43999 | A | 5 | 9 | 2 | SB | ||
L5247110-003 | 43999 | A | 3 | 2 | 2 | SB |
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 |
---|---|---|
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-S-763, CLASS 321, COND A FED SPEC SINGLE MATERIAL RESPONSE |
AAZR | MAJOR DIAMETER | 0.404 INCHES NOMINAL |
ASBP | BORE TYPE | SPLINED |
ABMK | OVERALL WIDTH | 0.562 INCHES NOMINAL |
BFHN | DISTANCE BETWEEN FORK INSIDE SPREAD | 0.437 INCHES NOMINAL |
AGJR | MINOR DIAMETER | 0.337 INCHES NOMINAL |
MATT | MATERIAL | STEEL |
BFGX | SHAFT END THICKNESS | 0.500 INCHES NOMINAL |
ABSA | SPLINE QUANTITY | 17 |
BFGY | LINK END THICKNESS | 0.625 INCHES NOMINAL |
AGAV | END ITEM IDENTIFICATION | B-1B ACFT; TRANSDUCER-LOWER RUDDER POSITION-FLIGHT AND AUX CONTROL |
CZLP | SHAFT SECURING METHOD | SPLINE |
BFHA | LINK END HOLE DIAMETER | 0.190 INCHES NOMINAL |