Mfg Part Number: R11223 | Manufacturer: Parker Hannifin Corp |
NSN : 2915-00-884-3285 | NIIN : 008843285 |
Item Name : manifold fuel | CAGE Code : 50599 |
FSC : 2915 Engine Fuel System Components Aircraft and Missile Prime Movers |
Thank you for your interest in our available R11223 NSN part. This part number R11223 is a Manifold Fuel listed under the FSC 2915 Engine Fuel System Components Aircraft and Missile Prime Movers, and it is manufactured by Parker Hannifin Corp. At Internet of Components, all of our stock and inventory are available for purchase today, ready to ship with short lead times and competitive pricing. Whether you are in need of parts that are new, used, or obsolete, our team of industry experts is readily available 24/7x365 to fulfill all of your operational
“*” Symbols for mandatory fields
Internet of Components is a premier supplier of R11223 NSN component, and we carry recently requested NSN components such as 2915008843285. We strive to only provide our customers with quality parts, which is why we choose to source our inventory from thousands of global manufacturers such as Parker Hannifin Corp. If you are interested in this particular item, we invite you to begin the purchasing process for R11223 today by filling out and submitting an Instant RFQ. Once received, a member of our staff will review and reach out to you in 15 minutes or less to provide a personalized quote that caters towards your individual needs. Get started on the purchasing process today and see how we are revolutionizing the purchasing process.
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 |
Don’t forget That If You’d Ever Like a Quote for Parts Within 15 Minutes or Less, You Can Fill out the Instant RFQ form On this Website’S Homepage.
Request for Quote