Thank you for taking an interest in part number HTS2-D, a San Antonio Air Logistics Center product we have in stock that is listed alongside the NSN 4920014341081 and the description “Test Stand Hydrauli.” As part number HTS2-D is readily available for purchase on our website at any time, you are invited to fill out and submit the RFQ form provided on this page for the means of requesting a quote for your comparisons. All that we ask is that you supply us with important information such as your target price and expected shipping time frame so that we can best tailor a solution that caters to your unique needs and restrictions alike.
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To ensure that you only procure the exact items you require for carrying out operations, we list all aerospace parts, military and defense parts, and other product offerings with all applicable information for identification. For example, part number HTS2-D is listed alongside the NSN 4920-01-434-1081, meaning that it also belongs to FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment. Furthermore, this NSN part is specifically manufactured under CAGE Code 98750, a unique identifier belonging to the manufacturer for a specific facility. With all of this in mind, kick off purchasing with us today and see why so many customers steadily choose us for their operational needs.
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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