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matt
200.0 ac
pump assembly: working psig 60.6, proof psig 120.0, burst 180.0; discharge valve & outlet flange: working PSIG120.0, proof psig 240.0, burst psig 360.0
aluminum alloy
hardened
nha: DAA3139B005, DAA3139B043, DAA3139M047; u/o: B-2 acft; useful life 30 years, operational life 20, 000 hours; medium: JP-4, JP-5, JP-8, JET-A, JET-B, JET-1, gasoline; no visible leakage external motor/pump elementwhile testing, electric power:ac, 200 volts, 400 hz
1EA
Aluminum alloy
Schedule B number: 8803300060
nmfc 128000
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.
pump assembly: working psig 60.6, proof psig 120.0, burst 180.0; discharge valve & outlet flange: working PSIG120.0, proof psig 240.0, burst psig 360.0 200.0 ac voltage in volts and current type
1. | DAA3272P035-227 | Cage 81205 |
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.