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For competitive procurement options on part number HTS2-D from Malabar (CAGE Code 94861), look no further than Just Parts Unlimited. With the form presented on this page, you can submit information on your needs to receive tailored procurement solutions from our staff.
Part Number HTS2-D Details:
Part number HTS2-D is manufactured by Malabar and listed with the item name Test Stand Hydrauli. Classified under NSN 4920-01-434-1081, the NIIN of this item is 014341081, its INC is 11017, and its NCB code is 01 (USA).
For organization and identification purposes, this item is listed within the Federal Supply Group (FSG) 49 Maintenance and Repair Shop Equipment and Class (FSC) 4920 Aircraft Maintenance And Repair Shop Specialized Equipment. These details are important for confirming parts before making a purchase.
Disclaimer: This is a quotation for the goods listed above. This quotation is meant as an estimate and does not reflect a final bill or invoice. All quotations are subject to change until acceptance by ASAP Semiconductor of a binding Purchase Order, and quotations may be withdrawn or revised at the sole discretion of ASAP Semiconductor. This quotation is subject to the ASAP Semiconductor Terms & Conditions available at https://www.asapsemi.com/terms-conditions.aspx . All United States Government and Department of Defense bids are quoted as CAGE code 6RE77 from ASAP Semiconductor’s Anaheim, California facility. Any quotation from ASAP Semiconductor without 6RE77 is void.
How to Get Started on 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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