Part Number
CAGE Information
| Code | Company |
|---|---|
| 99167 | HAMILTON SUNDSTRAND CORPORATION |
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 |
|---|---|---|
| TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | AMS 6440,HARDEN AND FREEZE,RC 58-62;FIRST END 0.2495 IN. MIN,0.2505 IN. MAX SPHERICAL RADIUS;SECOND END O.D. 0.370 IN. MIN,0.380 IN. MAX;SECOND END I.D. 0.209 IN. MIN,0.229 IN. MAX;HOLETHROUGH SECOND END 0.1908 IN. MIN,0.1912 IN. MAX DIA;DISTANCE BETWEEN SPHERE CENTER ON FIRST END AND CENTER OF SIDE HOLE ON SECOND END 3.026 IN. MIN,3.036 IN. MAX;ROD DIA BETWEEN ENDS 0.198 IN. MIN,0.208 IN. MAX |
| AGAV | END ITEM IDENTIFICATION | E-3A ACFT |