Rotable Parts Exchange serves as a comprehensive source for military products, aerospace equipment, and Manifold Fluid Aircraft items. You have expressed particular interest in part number 3-50931-1, a Northrop Grumman Technical Services Inc component we offer that is presented with the NSN 2995-00-884-3285 for straightforward identification and procurement. By completing and submitting the Request for Quote form provided on this page, you can obtain pricing details on this NSN part for your comparisons. Once our staff members receive and review your submitted information, a dedicated account manager will directly contact you with a response within 15 minutes or less.
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We strive to streamline the purchasing process and simplify it as much as possible, which includes providing detailed listings for all components to help customers pinpoint their exact needs. For instance, part number 3-50931-1 is manufactured by Northrop Grumman Technical Services Inc under the CAGE Code 0JRC1. Additionally, by using the initial digits of the NSN 2995-00-884-3285, you can discover that this component is associated with the FSC 2995 Miscellaneous Engine Accessories Aircraft. If you have any specific questions about our database, you may always give us a call or email, as we would be delighted to assist you however we can. Otherwise, we encourage you to secure a quote for part number 3-50931-1 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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