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F110-GE-129 aircraft engine; main engine control p/n 8062-920; t.o.6J3-4-120-4
serves as a cap to the sensor well of the compressor discharge pressuresensor and filter assembly p/n 6065-076; 1/4 inch tube connection facility provided; material ams 4215 (C355-T6) ; 4 mounting holes provides menas to attached to sensor housing p/n 4033-464
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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 aircraft engine;main engine control p/n 8062-920;t.o.6j3-4-120-4.