Rotable Parts Exchange serves as a comprehensive source for military products, aerospace equipment, and Manifold Fuel items. You have expressed particular interest in part number R11223, a Parker Hannifin Corporation component we offer that is presented with the NSN 2915-00-884-3285 for straightforward identification and procurement. By completing and submitting the Request for Quote form provided on this page, you can obtain pricing details on this NSN part for your comparisons. Once our staff members receive and review your submitted information, a dedicated account manager will directly contact you with a response within 15 minutes or less.
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We strive to streamline the purchasing process and simplify it as much as possible, which includes providing detailed listings for all components to help customers pinpoint their exact needs. For instance, part number R11223 is manufactured by Parker Hannifin Corporation under the CAGE Code 50599. Additionally, by using the initial digits of the NSN 2915-00-884-3285, you can discover that this component is associated with the FSC 2915 Engine Fuel System Components Aircraft and Missile Prime Movers. If you have any specific questions about our database, you may always give us a call or email, as we would be delighted to assist you however we can. Otherwise, we encourage you to secure a quote for part number R11223 at your earliest convenience.
| 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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