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A10A acft fuel system
designed for partially submerged operation, 200 v ac 400 hz 3 ph, 3000 phr at 24 psi rated capacity using JP-4 fuel, 8.030 in. lg, 7.582 in. w, 3.000 in. h o/a dim., 6 mtg holes, two holes 0.281 in. dia on flange on 1.812 in. ctrs, 4 holes 0.266 in. dia on square flange equispaced on 1.812 in. ctrs, 4 wire electrical lead unprocessed 36 in. lg, w/3 thermal protectors
On 12/02/1999 under contract F4160898D06610008 for qty 3
1EA
Schedule B number: 8803300060
nmfc 127600
Other parts of airplanes or helicopters for use in military aircraft (excludes propellers, rotors, undercarriages, and parts the
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 a10a acft fuel system.
1. | 385800-2 | Cage 59875 |
Nothing similar to this part number was found in our inventory
A completely inclosed machine consisting of a positive or nonpositive displacement pump with a driving motor used to transmit or transfer fluid from an aircraft tank to an engine driven pump or to another tank. it is designed to be partially or completely submerged in the fluid it is intended to pump.