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main fuel pump MFP-330 for F100-PW-100/-200 aircraft engine
cres per AMS5640, immunize per PSM903; flange 2.0751 - 2.0760 in. od 0.23 - 0.24 in. thk, 1.91 - 1.92 in. id, 0.15 in. dp; body 1.820 - 1.822 in. od, 0.36 - 0.37 in. lg, bore 1.65 - 1.66 in. dia; use on boost housing and insert assy, p/n 98607
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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 main fuel pump mfp-330 for f100-pw-100/-200 aircraft engine.