Part Number
Definition:
AN ASSEMBLY CONSISTING OF TWO OR MORE HYDRAULIC SERVOCYLINDERS ON A COMMON MOUNTING, WITH ONE OR MORE SERVOCYLINDERS PERFORMING A SEPARATE FUNCTION UNRELATED TO THE FUNCTION(S) OF THE REMAINING CYLINDER(S). EXCLUDES A SERVOCYLINDER WITH TWO OR MORE CYLINDERS WHICH PERFORMS A SINGLE FUNCTION.
CAGE Information
| Code | Company |
|---|---|
| 43999 | 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 |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | B1B ACFT |
| FEAT | SPECIAL FEATURES | E22.250 IN.APPROX.O/A LG;CONSISTS OF THE FOLLOWING:SERVOVALE 1;LINK ASSY.1;LEVER 1;SUPPORT 1;TUBE 2;COMPENSATOR 2;ROD END 2;COLLAR 1;FILTER 1;CYLINDER 1;TRANSDUCER 3;WIRE HARNESS 1;AND MISC.HARDWARE |