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aircraft engine fuel transfer system, p/n 53-58511
ured anodized finish, side mounted, 3.4 lbs max wt, electrically operated, 3 terminals size 10-32 NF-3A, 18 to 30 volts, direct current, 0.53 amps at 24 volts dc at 68 deg f, 200 gpm rated flow, 0 to 60 psig operating pressure, used in control of JP-4 or JP-5 fuels, o/a dim. approx 8.325 in. min to 8.385 in. max lg by approx 6.115 in. min to 6.235 in. max w, sq flange w/rounded corners, 4 steel inserts size 0.250-28 UNF-3B by 0.380 in. deep, recessed, spaced 1.812 in. c to c, 1.430 in. dia center
1EA
Schedule B number: 8481809050
nmfc 051080
Other taps, cocks, valves, etc.
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 aircraft engine fuel transfer system,p/n 53-58511.
1. | F59B0009M1 | Cage 92003 |
2. | 32-58030-38 | Cage 76301 |