You have arrived on the Request for Quote (RFQ) page for part number R11223, a Parker Hannifin Corporation component that is listed with the product description “Manifold Fuel” and NSN 2915-00-884-3285 for fast identification. By using the form supplied below, you can offer details regarding your requirements to secure customized procurement solutions for your consideration. As our goal is to provide quick service, you can expect a response within 15 minutes of our staff members reviewing your submission. Alternatively, if you use the email or phone number at the bottom of the webpage, you can directly connect with our experts to discuss your needs.
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Alongside Parker Hannifin Corporation part number R11223, you can seamlessly search for more items from this manufacturer or CAGECode 50599 using our curated catalogs. Similarly, we also offer means for locating other products that belong to FSC 2915 Engine Fuel System Components Aircraft and Missile Prime Movers, which this component falls under having the NSN 2915-00-884-3285. Whether you desire part number R11223 or other NSN components, you can rest assured that our entire inventory is sourced from reputable manufacturers and suppliers. Bearing this in mind, kick off procurement today to see why so many customers select Aero Defence Solutions as their trusted purchasing hub.
| 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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