Thank you for considering Malabar part number HTS2-D, a component we stock that is further identified by the NSN 4920-01-434-1081 and product description “Test Stand Hydrauli.” This item is currently available for purchase on our website today, and you can obtain a tailored quote at any time by completing the form on this page. To help us provide the best solution, please include critical details like your quantity requirements, target pricing, and delivery preferences within the submitted request. Once we receive your form, our team will promptly review provided information and respond with a quote that aligns with your needs.
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Alongside part number HTS2-D, we encourage you to explore other offerings we carry from Malabar that have been produced under CAGE Code 94861, as well as similar products classified under FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment that may suit your projects. We can help you obtain pricing on all items that you are interested in, securing the most optimal solution for you. We are also happy to discuss any requirements that you may have, presenting specialized options for many restrictions and needs alike. With our services in mind, please submit your request for part number HTS2-D today and discover why Marine Defence Parts is a trusted partner for naval and defense procurement.
| MRC | Criteria | Characteristic |
|---|---|---|
| CGYK | ENGINE DRIVEN HYDRAULIC PUMP TESTING DESIGN FEATURE | NOT INCLUDED |
| CHGR | PRESSURE/SUCTION HOSE | INCLUDED |
| CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | DIESEL DRIVEN POWERED DUAL SUB-SYSTEM TEST STAND |
| BGST | PRESSURE RATING | 3000.0 POUNDS PER SQUARE INCH MINIMUM AND 6000.0 POUNDS PER SQUARE INCH MAXIMUM |
| ATJK | POWER SOURCE | GASOLINE ENGINE |
| AYJM | ACCUMULATOR | INCLUDED |
| FEAT | SPECIAL FEATURES | USED FOR TYPE III; THE DRIVE SYSTEM IS THE ONLY PRIMARY DIFFERENCE FROMTHE ELECTRIC COUNTERPART |
| FTLD | III FUNCTIONAL DESCRIPTION | USED TO PRESSURIZE AIRCRAFT HYDRAULIC SYSTEM WITHOUT HAVING TO USE AIRCRAFT ENGINE OR AUXILARY POWER UNIT; THIS PRESSURIZATION ALLOWS FUNCTIONAL CHECK OF FLIGHT CONTROL SYSTEM/LANDING GEAR OPERATION PRIOR TO AIRCRAFT FLIGHTTO ENSURE NO MALFUNCTIONS ARE OCCURING |
| RDAL | III REFERENCE DATA AND LITERATURE | MIL-PRF-38381 |
| ALBY | USAGE DESIGN | AIRCRAFT HYDRAULIC SYSTEM |
| AMQY | INSTALLATION DESIGN | PORTABLE |
| AGAV | III END ITEM IDENTIFICATION | MULTI-ACFT |
| CHGQ | FILTERING SYSTEM | INCLUDED |
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