1534M52P16: FUEL CONTROL,MAIN,TURBINE ENGINE.
FUEL CONTROL,MAIN,TURBINE ENGINE. Key specifications include material: ALUMINUM ALLOY, end_item_identification: F110-GE-129 TURBO FAN AUGMENTED JET ENGINE, reference_data_and_literature: T.O.6J3-4-120-503;CONTROL,MAIN ENGINE;T.O.2J-F110-14,FIG.35, part_name_assigned_by_controlling_agency: CONTROL,MAIN ENGINE, reference_number_differentiating_characteristics: AS DIFFERENTIATED BY SOURCE CONTROL DRAWING. This part is cataloged in the U.S.
Government catalog under NSN 2915-01-448-3117, indicating validated use in U.S. government and defense logistics supply chains. Available through authorized enterprise resellers and TPM (Third Party Maintenance) channels.
Verify compatibility with your specific system configuration before ordering.
| material | ALUMINUM ALLOY |
| end_item_identification | F110-GE-129 TURBO FAN AUGMENTED JET ENGINE |
| reference_data_and_literature | T.O.6J3-4-120-503;CONTROL,MAIN ENGINE;T.O.2J-F110-14,FIG.35 |
| part_name_assigned_by_controlling_agency | CONTROL,MAIN ENGINE |
| reference_number_differentiating_characteristics | AS DIFFERENTIATED BY SOURCE CONTROL DRAWING |
| NSN | 2915-01-448-3117 |
| REFERENCE DATA AND LITERATURE | T.O.6J3-4-120-503;CONTROL,MAIN ENGINE;T.O.2J-F110-14,FIG.35 |
| 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 AND EXHAUST GAS TEMPERATURE WITH THE POSITION OF THE COCKPIT POWER CONTROL LEVER AND DEMANDS FROM THE ELECTRONIC ENGINE CONTROL SYSTEM |
| PART NAME ASSIGNED BY CONTROLLING AGENCY | CONTROL,MAIN ENGINE |
| END ITEM IDENTIFICATION | F110-GE-129 TURBO FAN AUGMENTED JET ENGINE |
| MATERIAL | ALUMINUM ALLOY |
| REFERENCE NUMBER DIFFERENTIATING CHARACTERISTICS | AS DIFFERENTIATED BY SOURCE CONTROL DRAWING |