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Thank you for taking an interest in the Fuel Control Main Turbine Engine NSN parts that we carry here on Buy Military Ground Vehicle Parts. You have reached the RFQ page for part number 1534M52, an item that traces back to the manufacturer General Electric Company. Listed with NSN 2915014483117, this listing is available for purchase from our website at any time. If you are interested in part number 1534M52 and wish to learn more, be sure to fill out and submit the RFQ form found on this page. By presenting us information such as your target price and expected delivery date, we can best formulate and present a solution that closely caters to your unique needs and restrictions alike.
| NSN | FSC | NIIN | CLS | Hazmat | DEMIL | Cancelled NSN |
|---|---|---|---|---|---|---|
| 2915-01-448-3117 Item PartTypeName: FUEL CONTROL,MAIN,TURBINE ENGINE | 2915 | 014483117 | 0 | N | ||
| CIIC | HCC | ESD | PMIC | Criticality | ENAC | |
| I | A | 0 | ||||
| Part Number | ISC | RNVC | RNCC | HCC | MSDS | SADC |
| 1534M52P16N | 1 | 9 | 5 |
| MRC | Criteria | Characteristic |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | F110-GE-129 TURBO FAN AUGMENTED JET ENGINE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | CONTROL,MAIN ENGINE |
| 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 A |
| MATT | MATERIAL | ALUMINUM ALLOY |
| RDAL | REFERENCE DATA AND LITERATURE | T.O.6J3-4-120-503;CONTROL,MAIN ENGINE;T.O.2J-F110-14,FIG.35 |
| ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY SOURCE CONTROL DRAWING |
| AGAV | END ITEM IDENTIFICATION | F110-GE-129 TURBO FAN AUGMENTED JET ENGINE |
| CXCY | PART NAME ASSIGNED BY CONTROLLING AGENCY | CONTROL,MAIN ENGINE |
| 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 A |
| MATT | MATERIAL | ALUMINUM ALLOY |
| RDAL | REFERENCE DATA AND LITERATURE | T.O.6J3-4-120-503;CONTROL,MAIN ENGINE;T.O.2J-F110-14,FIG.35 |
| ZZZY | REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY SOURCE CONTROL DRAWING |
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