Whether you are in search of military and defense parts, aerospace parts, or other similar product solutions, Satellite To Submarine Parts is your one-stop shop. Thank you for your interest in part number R11223, a Parker Hannifin Corporation item that is listed alongside the description “Manifold Fuel” and the NSN 2915008843285. To guarantee a swift procurement process for NSN part number R11223, be sure to request a quote by filling out and submitting the RFQ form below, and one of our experts will offer a customized solution for your comparisons in response.
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We list everything with as much relevant information as possible to ensure that customers can swiftly identify and procure the exact products they need. For instance, while part number R11223 is manufactured by Parker Hannifin Corporation, it is specifically done so under CAGE Code 50599, a unique identifier assigned to a particular facility by the DLA that supplies to various government or defense agencies. Additionally, using the first digits of the NSN 2915-00-884-3285, one can also determine that this part falls under FSC 2915 Engine Fuel System Components Aircraft and Missile Prime Movers. Keeping this in mind, initiate the purchasing process today to see why so many customers depend on us for the NSN items they require.
| 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 |
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