To receive competitive purchasing options on part number HTS2-D by Malabar, look no further than NSN Direct. For your reference, this item has the NSN 4920-01-434-1081 and is listed with the description “Test Stand Hydrauli.” If this matches your needs, we encourage you to fill out the partially-completed quote request form on this page to kick off procurement. By providing comprehensive information about your requirements, such as your desired quantity, pricing, and fulfillment speed, our experts can formulate the most fitting solutions for you. We want to ensure that this process is quick and effortless, so we routinely respond to requests within 15 minutes of receiving and reviewing them.
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In addition to our streamlined quotation service, we also aim to make the process of finding products simple. As such, if you require other Malabar parts produced under the CAGE Code 94861, you can peruse our manufacturer or CAGE Code catalogs, or use our search engine and filters. Furthermore, if you want to locate items similar to part number HTS2-D, you can glean from the first four digits of its NSN 4920-01-434-1081 that it belongs to the FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment. This being said, do not hesitate to request quotes on part number HTS2-D and any other NSN parts that we feature to experience unrivaled 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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