Aerospace Engineering Solutions is proud to offer immediate purchasing options on Moog Inc part number 912484-2-1, a Test Stand Electric product we carry that is listed with the NSN 4920-01-320-9519 for ease of identification. If you would like to learn more about this item, be sure to complete the Request for Quote (RFQ) form provided on this page. By including essential details like your target price, desired quantity, and expected fulfillment timeline, you are ensured a fully customized quote from our team.
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For your reference, this product is traceable to Moog Inc through the CAGE Code 0ZWK8, as well as categorized under FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment based on the first four digits of the NSN 4920-01-320-9519. Using such information, you can easily narrow down exact items of need for an ease of procurement. With our quotation service in mind, be sure to submit a completed form when you are ready to begin. Should you wish to speak with one of our representatives to discuss services, you can also give us a call or email at your convenience. With all that we offer, choose Aerospace Engineering Solutions for part number 912484-2-1 and other NSN items of need.
| MRC | Criteria | Characteristic |
|---|---|---|
| CHGR | PRESSURE/SUCTION HOSE | NOT INCLUDED |
| AKCV | DRIVE TYPE | HYDRAULIC MOTOR |
| CGYK | ENGINE DRIVEN HYDRAULIC PUMP TESTING DESIGN FEATURE | INCLUDED |
| CGYL | FLOW CAPACITY RATING | 15.8 GALLONS PER MINUTE |
| CGYM | PRESSURE MANIFOLD SUBCIRCUIT | NOT INCLUDED |
| AAYJ | HYDRAULIC FLUID FLOW RATE | 35.0 GALLONS PER MINUTE |
| ATJK | POWER SOURCE | ELECTRIC MOTOR OR MANUAL |
| SR-5 | MANUFACTURERS CODE | 0ZWK8 |
| FEAT | SPECIAL FEATURES | C/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 |
| BJDW | MAXIMUM OPERATING PRESSURE | 4600.0 POUNDS PER SQUARE INCH |
| FTLD | III FUNCTIONAL DESCRIPTION | USED TO CHECK OUT THE LEADING EDGE FLAP,POWER DRIVE UNIT |
| FREQ | FREQUENCY IN HERTZ | 60.0 |
| AYJM | ACCUMULATOR | NOT INCLUDED |
| SR-5 | THE MANUFACTURERS DATA | |
| NTRD | III ENTRY DATE | 90-05-21 |
| FCLS | III FUNCTIONAL CLASSIFICATION | AA-9.2 |
| ELEC | VOLTAGE IN VOLTS | 115.0 |
| BGST | PRESSURE RATING | 4600.0 POUNDS PER SQUARE INCH NOMINAL |
| AGAV | III END ITEM IDENTIFICATION | POWER DRIVE UNIT,P/N 2022070 AND 2048666,USED ON THE F-16A/B/C/D/ |
| RDAL | III REFERENCE DATA AND LITERATURE | SERD-14025 |
| FAAZ | PHASE | SINGLE |
| ALBY | USAGE DESIGN | AIRCRAFT HYDRAULIC SYSTEM |
| ACDC | CURRENT TYPE | AC |
| ATPR | MAXIMUM SPEED RATING IN RPM | 150.0 |
| AMQY | INSTALLATION DESIGN | FIXED |
| CHGQ | FILTERING SYSTEM | INCLUDED |
| SR-5 | DESIGN CONTROL REFERENCE | 912484-2-1 |
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