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geae commercial aircraft engines
the stator comprises epoxy bonded laminations and dual three phase windings; an aluminum housing locates the stator and interfaces with the mounting pad; LOAD-Speed characteristics, rpm, voltage, amps, 2330, short circuit, 12.5 arms max, 2330, 20.8vrms, 6.32 arms, 2330, 31.3 vrms, open circuit; overspeed, 24272 for 1 min; electrical, DUAL-Redundant 3 phase wye windings; weight, stator 5.20 pounds max; temperature, -65 degrees f to 350 degrees f; cooling, convection; altitude, 0 to 50, 000 ft; compliance, MIL-STD-461B, MIL-STD-462, MIL-STD-810D, MIL-STD-204D; the alternator is gear driven from an engine accessory gear box; model 5318 provides electrical power for a fadec system used on several geae commercial aircraft engines
Schedule B number: 8411997050
Parts of gas turbine aircraft engines, other than for use in civil aircraft
FSC 2925 ⁓ Engine electrical system components, aircraft prime moving
Note-items designed for specific use on aircraft and guided missile prime movers are to be placed in this fsc.
Excluding aircraft lighting fixtures (fsc 6220); auxiliary aircraft generators (fsc 6115).
Used on geae commercial aircraft engines. the stator comprises epoxy bonded laminations
Nothing similar to this part number was found in our inventory
A stator which is a maintenance part of a generator, engine accessory.