You have reached the quote request page for part number R11223 of Parker Hannifin Corporation, we have in stock that is listed alongside the description Manifold Fuel. If you would like to learn more about this NSN part and your purchasing options, please fill out and submit the Request the Quote (RFQ) page presented on this page. By offering us important details like your target price and expected fulfillment time frame, our team can best offer you a tailored solution for your consideration. As we have staff available at all times, responses to any submission will be offered within 15 minutes of our review.
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To make exploring our expansive inventory simple, we have chosen to list all offerings alongside as much information as we can for an ease of identification. For example, part number R11223 is specifically produced under CAGE Code 50599, denoting the specific Parker Hannifin Corporation facility it traces back to. Furthermore, with the NSN 2915-00-884-3285, this item also belongs to FSC 2915 Engine Fuel System Components Aircraft and Missile Prime Movers, further ensuring that you only purchase your exact needs. If you have any questions or concerns regarding our offerings or service, be sure to call or email us at your convenience. Otherwise, we look forward to serving you as your strategic sourcing partner for part number R11223 and more.
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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