Thank you for taking interest in Malabar part number HTS2-D, which is listed with the NSN 4920-01-434-1081 and a product description of “Test Stand Hydrauli.” In order to receive procurement options on this particular listing, we ask that you fill out and submit the form provided below with as much information as you can concerning your needs. By supplying our staff with key details on your desired quantity, pricing target, and expedited fulfillment timeframe, we can respond with a quote that has been specifically tailored to your unique specifications. We also ask that you make us aware of any restrictions that you may have as soon as possible, such as if you have a time constraint or are seeking unlisted items.
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Alongside part number HTS2-D, you are encouraged to continue exploring our collection curated catalogs to find additional items that can accompany this Test Stand Hydrauli part with the NSN 4920-01-434-1081. For example, you can browse other Malabar components that were produced under CAGE Code 94861 or listings that belong to FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment with ease on our website, with search tools provided for quick location. Furthermore, our staff is just a call or email away from assisting you with any inquiries or requests, so be sure to get started on the quotation process for part number HTS2-D and other desired offerings on Aerospace Spare.
| 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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