Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 26002, a Malabar item with the NSN 4920014341081 that is listed alongside the description “Test Stand Hydrauli.” If you are interested in part number 26002 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 26002 is specifically listed with the NSN 4920-01-434-1081, and this code can be used to determine that it falls under FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment. Additionally, while tracing back to Malabar, this NSN part was specifically produced under CAGE Code 94861. With our services and dedication to simple procurement in mind, get started with us today!
| 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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