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F110-GE-129 turbo fan augmented jet engine
control, main engine
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
aluminum alloy
t.o.6J3-4-120-503; control, main engine; t.o.2J-F110-14, fig.35
as differentiated by source control drawing
1EA
Aluminum alloy
Schedule B number: 8411997050
nmfc 133300
Parts of gas turbine aircraft engines, other than for use in civil aircraft
FSC 2915 ⁓ Engine fuel system components, aircraft and missile prime movers
Note-fuel components specially designed for propulsion fuel systems, aircraft and missiles are to be placed in this fsc.
Excluding aircraft fuel tanks (fsc 1560); in-flight refueling system fuel components (fsc 1680). fuel system components not specifically designed for use with aircraft engines or missile prime-movers.
Used on f110-ge-129 turbo fan augmented jet engine. control, main engine
1. | 8062-928 | Cage 66503 |
2. | 1534M52P16N | Cage 07482 |
3. | 1534M52 | Cage 07482 |
Nothing similar to this part number was found in our inventory
A self contained metering unit consisting primarily of pumping, controlling, valving, and/or governing components. it is designed for regulating the delivery of fuel into the main fuel system of a turbine engine.