Thank you for taking an interest in the various military and defense parts, aerospace parts, and other items that we offer. You have reached the RFQ page for part number 1534M52, a General Electric Company item with the NSN 2915014483117 that is listed alongside the description “Fuel Control Main Turbine Engine.” If you are interested in part number 1534M52 and wish to learn more about your purchasing options, be sure to submit the form below at your earliest convenience while supplying us with important information concerning your needs and restrictions alike. Once we have a chance to receive and review your completed form, a member of our staff will reach out to you in 15 minutes or less to present a tailored solution for your comparisons.
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To ensure that shopping with us is as simple as possible, we make it easy to identify and procure exact items by listing parts alongside all applicable designations and information. For example, part number 1534M52 is specifically listed with the NSN 2915-01-448-3117, and this code can be used to determine that it falls under FSC 2915 Engine Fuel System Components Aircraft and Missile Prime Movers. Additionally, while tracing back to General Electric Company, this NSN part was specifically produced under CAGE Code 07482. With our services and dedication to simple procurement in mind, get started with us today!
| 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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