Thank you for taking interest in the Northrop Grumman Systems Corporation part number 3-50931-1, a Manifold Fluid Aircraft product that we stock that is presented alongside the NSN 2995-00-884-3285 for ease of identification. If you would like to learn more about this component and secure purchasing options for your consideration, please fill out and submit the Request for Quote (RFQ) form that is offered below. All we ask is that you supply us with enough information to best accommodate any particular requirements or restrictions that you may have, and we will respond with a curated quote within 15 minutes of our receipt and review.
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We strive to ensure that customers only receive precise items of need, opting to arrange our collection by diverse, commonly recognized forms of data. For instance, part number 3-50931-1 specifically traces back to Northrop Grumman Systems Corporation through the CAGE Code 76823, a distinct identifier for one of their physical locations. Moreover, with the NSN 2995-00-884-3285, this listing falls within Federal Supply Code (FSC) 2995 Miscellaneous Engine Accessories Aircraft, enabling one to figure out its basic application. Keeping this in mind, do not hesitate to obtain a competitive quote for part number 3-50931-1 here on Aero OEM Parts at your earliest convenience.
| 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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