You have arrived on the Request for Quote (RFQ) page for part number HTS2-D, a Malabar component that is listed with the product description “Test Stand Hydrauli” and NSN 4920-01-434-1081 for fast identification. By using the form supplied below, you can offer details regarding your requirements to secure customized procurement solutions for your consideration. As our goal is to provide quick service, you can expect a response within 15 minutes of our staff members reviewing your submission. Alternatively, if you use the email or phone number at the bottom of the webpage, you can directly connect with our experts to discuss your needs.
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Alongside Malabar part number HTS2-D, you can seamlessly search for more items from this manufacturer or CAGECode 94861 using our curated catalogs. Similarly, we also offer means for locating other products that belong to FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment, which this component falls under having the NSN 4920-01-434-1081. Whether you desire part number HTS2-D or other NSN components, you can rest assured that our entire inventory is sourced from reputable manufacturers and suppliers. Bearing this in mind, kick off procurement today to see why so many customers select Aero Defence Solutions as their trusted purchasing hub.
| 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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