NSN 4920-01-320-9519

Part Details | ELECTRIC AND HYDRAULIC SYSTEM COMPONENTS TEST STAND

4920-01-320-9519 A cabinetlike item usually with a front work area and consisting of the necessary instrumentation and mechanical and electrical facilities for component mounting. Designed to simultaneously test efficiency of packaged hydraulic pressure and electric power generating equipment. Component under test is equipped with self-contained power source. Excludes TEST STAND, HYDRAULIC SYSTEM COMPONENTS.

Alternate Parts: 91248421, 912484-2-1, 91248421, 912484-2-1, 4920-01-320-9519, 01-320-9519, 4920013209519, 013209519

Supply Group (FSG) NSN Assigned NIIN Item Name Code (INC)
49JUN 06, 199001-320-951961224 ( TEST STAND, ELECTRIC AND HYDRAULIC SYSTEM COMPONENTS )
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 4920-01-320-9519
Part Number Cage Code Manufacturer
912484-2-170210HONEYWELL INTERNATIONAL INC.DBA HONEYWELL
912484-2-10ZWK8MOOG INC.DBA MOOG AIRCRAFT GROUP TORRANCE
Technical Data | NSN 4920-01-320-9519
Characteristic Specifications
INSTALLATION DESIGN FIXED
USAGE DESIGN AIRCRAFT HYDRAULIC SYSTEM
PRESSURE RATING4600.0 POUNDS PER SQUARE INCH NOMINAL
HYDRAULIC FLUID FLOW RATE35.0 GALLONS PER MINUTE
ENGINE DRIVEN HYDRAULIC PUMP TESTING DESIGN FEATURE INCLUDED
DRIVE TYPE HYDRAULIC MOTOR
FLOW CAPACITY RATING15.8 GALLONS PER MINUTE
MAXIMUM OPERATING PRESSURE4600.0 POUNDS PER SQUARE INCH
MAXIMUM SPEED RATING IN RPM150.0
POWER SOURCED$DBZ
CURRENT TYPE AC
VOLTAGE IN VOLTS115.0
FREQUENCY IN HERTZ60.0
PHASE SINGLE
PRESSURE MANIFOLD SUBCIRCUIT NOT INCLUDED
ACCUMULATOR NOT INCLUDED
FILTERING SYSTEM INCLUDED
PRESSURE/SUCTION HOSE NOT INCLUDED
SPECIAL FEATURESC/O THREE SEPARATE UNITS,INTERFACED TO ONE ANOTHER BY ELECTRICAL CABLES; FIRST UNIT IS A HYDRAULIC TEST BENCH,DIM. 90.000 IN. W; 50.000 IN. D; 55.000 IN. H; WEIGHT: 5000 LBS; THE SECOND UNIT IS A INSTRUMENTATION AND CONTROL CONSOLE,DIM. 62.000 IN. H; 40.000 IN. W; 40.000 IN. D; WEIGHT: 500 LBS; POWER: 115 V,60 HZ,SINGLE PHASE 20 AMPS; THE THIRD UNIT IS A COMPUTER AND PRINTER,DIM. ON THE CRT ARE 18.000 IN. H; 18.000 IN. W; 7.000 IN. D; THE DIM. ON THE KEYBOARD ARE 3.000 IN. H; 18.000 IN. W; 7.000 IN. D
FUNCTIONAL CLASSIFICATIONAA-9.2
FUNCTIONAL DESCRIPTIONUSED TO CHECK OUT THE LEADING EDGE FLAP,POWER DRIVE UNIT
REFERENCE DATA AND LITERATURESERD-14025
ENTRY DATE90-05-21
END ITEM IDENTIFICATIONPOWER DRIVE UNIT,P/N 2022070 AND 2048666,USED ON THE F-16A/B/C/D/