Thank you for considering Parker Hannifin Corporation part number R11223, an item we carry that is listed with the NSN 2995-00-884-3285 and product description “Manifold Fluid Aircraft.” This component is available for purchase through our website at this time, so complete the Request for Quote (RFQ) form provided below if you would like to receive pricing information for your comparisons. Simply offer our staff details like your desired quantity, budget, and delivery timeline to help us craft the best solution for your needs.
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We aim to make the process of locating and procuring exact items simple, which is why we feature key listing details with every offering. For example, part number R11223 was specifically produced by Parker Hannifin Corporation under CAGE Code 50599, and with the NSN 2995-00-884-3285, it belongs to FSC 2995 Miscellaneous Engine Accessories Aircraft. Additionally, all stock comes delivered with any applicable qualifying certifications or manufacturer trace documentation for your further benefit. With all of this in mind, be sure to submit a request for part number R11223 today, knowing we will be in touch shortly after reviewing your information.
NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
---|---|---|---|---|---|---|
2995-00-884-3285 Item PartTypeName: MANIFOLD,FLUID,AIRCRAFT | 2995 | 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 |
---|---|---|
AGAV | END ITEM IDENTIFICATION | T-38A AIRCRAFT ENGINE |
CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | MANIFOLD,ENGINE FUEL,RH ENG |
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 |
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 |
FTLD | FUNCTIONAL DESCRIPTION | USED TO DIRECT FUEL TO THE MAIN AND AFTERBURNER FUEL PUMPS OF A TURBO JET ENGINE |
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