| INSTALLATION DESIGN | PORTABLE |
| USAGE DESIGN | AIRCRAFT HYDRAULIC SYSTEM |
| PRESSURE RATING | 6000.0 POUNDS PER SQUARE INCH NOMINAL |
| HYDRAULIC FLUID FLOW RATE | 60.0 GALLONS PER MINUTE |
| ENGINE DRIVEN HYDRAULIC PUMP TESTING DESIGN FEATURE | INCLUDED |
| DRIVE TYPE | ELECTRIC MOTOR |
| FLOW CAPACITY RATING | 30.0 GALLONS PER MINUTE |
| MAXIMUM OPERATING PRESSURE | 6000.0 POUNDS PER SQUARE INCH |
| MAXIMUM SPEED RATING IN RPM | 3600.0 |
| POWER SOURCE | ELECTRIC MOTOR |
| HORSEPOWER RATING | 40.0 |
| CURRENT TYPE | AC |
| VOLTAGE IN VOLTS | 440.0 |
| FREQUENCY IN HERTZ | 60.0 |
| PHASE | THREE |
| PRESSURE MANIFOLD SUBCIRCUIT | INCLUDED |
| SUBCIRCUIT QUANTITY AND MAXIMUM OPERATING PRESSURE | ONE 50 PSI |
| CIRCUIT TYPE | BOOSTER CYLINDER |
| CIRCUIT PRESSURE RATING | 50.0 POUNDS PER SQUARE INCH NOMINAL |
| ACCUMULATOR | NOT INCLUDED |
| FILTERING SYSTEM | INCLUDED |
| PRESSURE/SUCTION HOSE | INCLUDED |
| FUNCTIONAL CLASSIFICATION | AA-9.2 |
| FUNCTIONAL DESCRIPTION | USED TO TEST AIRCRAFT HYDRAULIC SYSTEMS/COMPONENTS WITHOUT OPERATING AIRCRAFT OR REMOVING COMPONENTS |
| RELATIONSHIP TO SIMILAR EQUIPMENT | REFURBISHED 4920-01-044-5926 |
| REFERENCE DATA AND LITERATURE | TO 33D2-5-39-1 |