Welcome to our online Request for Quote (RFQ) service, where you can fill out and submit the form provided below to obtain tailored procurement options from our team of industry experts. You have taken interest in part number R11223, which is a Manifold Fuel item from Parker Hannifin Corporation that is listed with the NSN 2915-00-884-3285 for quick identification. Should you wish to move forward with quotation for this listing, be sure that you supply us with key details like your target pricing, quality, and delivery date. This information is what we will base presented quotes on, with responses offered shortly after the receipt and review of each form.
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To ensure that customers only procure exact items of need, we present our offerings with as much relevant data as possible. For example, part number R11223 was specifically produced by Parker Hannifin Corporation under the CAGE Code 50599, providing traceability. Furthermore, with the NSN 2915-00-884-3285, one can also determine that this listing falls under Federal Supply Class (FSC) 2915 Engine Fuel System Components Aircraft and Missile Prime Movers. Alongside such details, all purchases will come delivered with any applicable qualifying certifications, furthering the reliability of our purchasing options. With this in mind, be sure to request a quote on part number R11223, and we will be in touch.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2915-00-884-3285 Item Description: MANIFOLD,FUEL | 2915 | 008843285 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| U | A | |||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| R11223 | 6 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| CXCY | Part Name Assigned By Controlling Agency | MANIFOLD,ENGINE FUEL,RH ENG |
| MRC | Decoded Requirement | Clear Text Reply |
| FTLD | Functional Description | USED TO DIRECT FUEL TO THE MAIN AND AFTERBURNER FUEL PUMPS OF A TURBO JET ENGINE |
| SUPP | Supplementary Features | FUEL PRESSURE WILL BE 50 PSIG,FLUID TEMPERATURE WILL RANGE FROM -65F TO 110F,AMBIENT TEMPERATURE WILL RANGE FROM -65F TO 200F |
| AGAV | End Item Identification | T-38A AIRCRAFT ENGINE |
| FEAT | Special Features | NO FLAMMABLE MATERIALS SHALL BE USED. DISSIMILAR METALS SHALL NOT BE USED. METALLIC SURFACES SHALL BE TREATED I/A/W MIL-F-7179 |
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