Part Number
Definition:
A RIGID ITEM OF VARIOUS SHAPES AND CROSS-SECTIONS, SPECIFICALLY DESIGNED TO MANUALLY ACTUATE AND/OR REGULATE A VARIETY OF MECHANISMS. IT USUALLY HAS AN INTEGRAL HANDGRIP, KNOB, OR THE LIKE, OR PROVISIONS FOR THE MOUNTING OF THE SAME. IT MAY HAVE ACCOMMODATIONS FOR LOCKING AND/OR POSITIONING. THE POINT OF FULCRUM MAY BE AN INTEGRAL SHAFT PERPENDICULAR TO THE AXIS OR A THROUGH HOLE TO PROVIDE A DEFINITE MEANS OF SECURING, AND USUALLY HAS ADDITIONAL ACCOMMODATION(S) FOR ATTACHMENT OF CONNECTING LINK, RIGID; WIRE ROPE ASSEMBLY, SINGLE LEG; AND CLEVIS, ROD END; ETC.. EXCLUDES ARM (AS MODIFIED); LEVER, REMOTE CONTROL; AND BELL CRANK.
CAGE Information
| Code | Company |
|---|---|
| 18355 | BOEING COMPANY THE DBA BOEING DIV DE |
Federal Supply Class
Title
AIRCRAFT HYDRAULIC, VACUUM, AND
Inclusions:
INCLUDES HYDRAULIC AND PNEUMATIC ACCUMULATORS, PUMPS, MOTORS, ACTUATING CYLINDERS, AND FILTERS; DE-ICING BOOTS; FLUID TYPE DE-ICING PUMPS, VALVES AND FILTERS; VACUUM SYSTEM OIL SEPARATORS; PNEUMATIC PRESSURIZATION EQUIPMENT OTHER THAN THAT FOR PRESSURIZING CABINS AND COMPARTMENTS.
Exclusions:
EXCLUDES JET ENGINE HYDRAULIC COMPONENTS (FSC 2840); VALVES SPECIFICALLY DESIGNED FOR AIR CONDITIONING, HEATING, VENTILATING, CABIN PRESSURIZING, AND THERMAL DE-ICING (FSC 1660); VALVES SPECIFICALLY DESIGNED FOR USE WITH AIRCRAFT ENGINES (FSC 2840); GUIDED MISSILES AND GUIDED MISSILE ENGINES (FSC 1338), LANDING GEAR (FSC 1620), WHEEL AND BRAKE SYSTEM COMPONENTS (FSC 1630); OXYGEN BREATHING SYSTEM COMPONENTS (FSC 1660); IN-FLIGHT REFUELING SYSTEM HYDRAULIC COMPONENTS (FSC 1680); SPECIFICALLY DESIGNED HYDRAULIC POWER STEERING SYSTEM COMPONENTS (FSC 1620).
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| FEAT | SPECIAL FEATURES | STEEL;SHAFT END 0.375 IN. DIA,36 SERRATIONS,1.437 IN. TO CORNER OF ARM;ARM END CONE SHAPED,0.219 SPHERICAL DIAMETER |