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 ST523912, a Hamilton Sundstrand Corporation item with the NSN 4920011484144 that is listed alongside the description “Flow Test Bench Fue.” If you are interested in part number ST523912 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 ST523912 is specifically listed with the NSN 4920-01-148-4144, 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 Hamilton Sundstrand Corporation, this NSN part was specifically produced under CAGE Code 55820. With our services and dedication to simple procurement in mind, get started with us today!
MRC | Criteria | Characteristic |
---|---|---|
SR-5 | MANUFACTURERS CODE | 66195 |
SR-5 | DESIGN CONTROL REFERENCE | ST523912 |
SR-5 | THE MANUFACTURERS DATA | |
AGAV | III END ITEM IDENTIFICATION | JET FUEL STARTER ASSY,F-16A/B |
TEXT | GENERAL CHARACTERISTICS ITEM DESCRIPTION | C/O A CHAMBER W/GLASS FRONT. ON THE FLOOR OF THE CHAMBER ARE LOCATED SIX PORTS THAT ALIGN W/SIX EJECTORS OF THE FUEL MANIFOLD ASSY. THE PORTS FUNNEL TEST FLUID TO INDIVIDUAL BEAKERS ADAPTED TO BOTH THE FUEL MANIFOLD AND THE START NOZZLE. UTILIZES A VARIABLE DISPLACEMENT VANE-TYPE PUMP TO PROVIDE TEST FLUID AT DESIRED PRESSURES AND FLOWS; ELEC RQMTS: 110V,15A; 240V 30,30A; TEST FLUID: STODDARD SOLVENT PER MIL-C-7024,TYPE II; PRESSURE: 450 PSIG MAX.; FLOW: 980 PPH MAX |
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