Thank you for taking an interest in part number 9398M83P19, a General Electric Company product we have in stock that is listed alongside the NSN 2915014480588 and the description “Fuel Control Main Turbine Engine.” As part number 9398M83P19 is readily available for purchase on our website at any time, you are invited to fill out and submit the RFQ form provided on this page for the means of requesting a quote for your comparisons. All that we ask is that you supply us with important information such as your target price and expected shipping time frame so that we can best tailor a solution that caters to your unique needs and restrictions alike.
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To ensure that you only procure the exact items you require for carrying out operations, we list all aerospace parts, military and defense parts, and other product offerings with all applicable information for identification. For example, part number 9398M83P19 is listed alongside the NSN 2915-01-448-0588, meaning that it also belongs to FSC 2915 Engine Fuel System Components Aircraft and Missile Prime Movers. Furthermore, this NSN part is specifically manufactured under CAGE Code 07482, a unique identifier belonging to the manufacturer for a specific facility. With all of this in mind, kick off purchasing with us today and see why so many customers steadily choose us for their operational needs.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2915-01-448-0588 Item PartTypeName: FUEL CONTROL,MAIN,TURBINE ENGINE | 2915 | 014480588 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| I | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 9398M83 | 1 | 9 | D |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | F110-GE-100 TURBO FAN AUGMENTED JET ENGINE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | MAIN ENGINE CONTROL |
| FTLD | FUNCTIONAL DESCRIPTION | FUEL-METERING DEVICE USED ON TURBINE ENGINES THAT METERS THE PROPER QUANTITY OF FUEL TO BE FED INTO THE COMBUSTION CHAMBERS OF THE ENGINE.IT INTEGRATES THE PARAMETERS OF INLET AIR TEMPERATURE, COMPRESSOR SPEED, COMPRESSOR DISCHARGE PRESSURE |
| MATT | MATERIAL | ALUMINUM ALLOY |
| RDAL | REFERENCE DATA AND LITERATURE | T.O.6J3-4-115-513 (TCTO);2J-F110-4,F.20,I.113 |
| ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY SOURCE CONTROL DRAWING |
| AGAV | END ITEM IDENTIFICATION | F110-GE-100 TURBO FAN AUGMENTED JET ENGINE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | MAIN ENGINE CONTROL |
| FTLD | FUNCTIONAL DESCRIPTION | FUEL-METERING DEVICE USED ON TURBINE ENGINES THAT METERS THE PROPER QUANTITY OF FUEL TO BE FED INTO THE COMBUSTION CHAMBERS OF THE ENGINE.IT INTEGRATES THE PARAMETERS OF INLET AIR TEMPERATURE, COMPRESSOR SPEED, COMPRESSOR DISCHARGE PRESSURE |
| MATT | MATERIAL | ALUMINUM ALLOY |
| RDAL | REFERENCE DATA AND LITERATURE | T.O.6J3-4-115-513 (TCTO);2J-F110-4,F.20,I.113 |
| ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY SOURCE CONTROL DRAWING |
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