Thank you for your interest in NSN part number R11223 under NSN 2915008843285 on Click Aerospace. Click Aerospace is a website owned and operated by ASAP Semiconductor, offering customers access to an unparalleled inventory of premium parts that cater to a variety of industries and applications. Manifold Fuel is an item listed with the part number R11223, and FSC 2915 Engine Fuel System Components Aircraft and Missile Prime Movers and it is manufactured by Smiths Tubular Systems Laconia Inc having CAGE Code 78570. This item, alongside the rest of our listed NSN parts, is readily available for purchase through our website now. Get started on the purchasing process today by filling out and submitting an Instant RFQ as provided through our website. Once received, a member of our staff will reach out to you in 15 minutes or less to offer a personalized quote based on your individual needs.
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Click Aerospace is a leading independent distributor of NSN part R11223, and we can help you procure NSN components such as 2915008843285 and many more. The quality of our inventory is of the utmost importance to us, and thus we choose to only source our parts from global manufacturers like Smiths Tubular Systems Laconia Inc. Get started with a competitive quote today when you submit an Instant RFQ and experience how we are revolutionizing the parts procurement process.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2915-00-884-3285 Item Description: MANIFOLD,FUEL | 2915 | 008843285 | 9387.10 | N | N | |
CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
0 | FUEL | A | ||||
Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
R11223 | 6 | 1 | C | 9 |
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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