1534M52 by General Electric Company - Receive a Competitive Quote
| Part Number: 1534M52 | Manufacturer: General Electric Company | NSN : 2915-01-448-3117 | Item Name : Fuel Control Main Turbine Engine | CAGE Code: 07482 | FSC : 2915 Engine Fuel System Components Aircraft and Missile Prime Movers | ||
We’re excited to announce that 1534M52 NSN part is now available and ready for immediate shipping. Part number 1534M52 is a Fuel Control Main Turbine Engine manufactured by General Electric Company with NSN 2915014483117. Are you interested in a quick and competitive quote for this part?
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NSN Information for Part Number 1534M52 with NSN 2915-01-448-3117, 2915014483117
| 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 |
| 8062-928 | 1 | 3 | 3 |
Characteristics Data of NSN 2915-01-448-3117, 2915014483117
| 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 |
