We appreciate your interest in part number ST523912, which is currently available for purchase here on Jet Force Aero. For your reference, this item is produced by Solar Turbines Incorporated and is listed with the NSN 4920-01-148-4144, as well as the description “Flow Test Bench Fue.” If this matches your requirements, we encourage you to fill out the Request for Quote (RFQ) form featured on this page to receive tailored purchasing options on part number ST523912. All that we ask is that you submit as many details about your procurement needs as possible, such as your desired quantity, budget, and anticipated fulfillment timeframe, as this will enable our specialists to craft an ideal response for you.
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In addition to part number ST523912, be sure to explore our website further for related items produced by Solar Turbines Incorporated under the CAGE Code 66195 as you wish. We also feature catalogs to help you find additional options that are categorized under FSC 4920 Aircraft Maintenance And Repair Shop Specialized Equipment and the NSN 4920-01-148-4144. Regardless of which NSN parts you need from us, rest assured that we will always treat you to affordable solutions where you never have to sacrifice quality or prompt fulfillment. We are ready to assist you with all your sourcing needs, so kick off quotation at your convenience.
| 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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