Aerospace Performance Parts is pleased to offer immediate purchasing options for General Electric Company part number 1534M52, which you have taken interest in. This Fuel Control Main Turbine Engine item is listed alongside the NSN 2915-01-448-3117 for ease of identification, with various additional information provided on this page for your reference. Should you wish to obtain solutions on this particular listing, we invite you to complete the Request for Quote (RFQ) form on this page at your earliest convenience. Responses are always offered shortly after we receive and review each request, with solutions we give being fully based on the details we are provided.
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If you happen to require expedited shipping for part number 1534M52 or any other FSC 2915 Engine Fuel System Components Aircraft and Missile Prime Movers components we carry from General Electric Company under CAGE Code 07482, be sure to let us know as soon as possible. We would be happy to discuss the options that we can potentially provide, our track record of on-time delivery being a testament to our dedication to customer satisfaction. You can either include such details within your request, or get in touch with staff directly. Otherwise, request a quote on NSN 2915-01-448-3117 part number 1534M52 today, knowing we will support all your operational needs with care.
| 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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