Generator Rotors

41 part numbers
570365 NSN 2925-00-059-7991 Cross Reference: 42828
  • 0.9062 inches overall length
  • 2.1150 inches overall diameter
  • shaft features provided
  • slot wound construction
47254-2 NSN 2925-00-118-4887
  • 4.3750 inches overall length
  • 4.3120 inches overall diameter
  • shaft features provided
  • squirrel cage construction
4020242 NSN 2925-00-327-6212 Cross Reference: 48410
  • 2.6870 inches overall length
  • 0.6262 inches overall diameter
  • shaft features provided
  • permanent magnet construction
10-383192-1 NSN 2925-00-461-4954
  • 4.4330 inches overall length
  • 2.5000 inches overall diameter
  • bearing and shaft features provided
  • salient pole construction
4009T36P01 NSN 2925-00-578-4068 Cross Reference: 36C715795G01
  • 2.6190 inches overall length
  • 2.4180 inches overall diameter
  • salient pole construction
513786 NSN 2925-00-999-3363 Cross Reference: 75320
  • 1.9060 inches overall length
  • 1.5200 inches overall diameter
  • shaft features provided
  • salient pole construction
49574 NSN 2925-01-148-4295 Cross Reference: 9974M83P01
  • u/o f108cf100 engine, e/i kc135 r aircraft end application
9334M40P01 NSN 2925-01-150-2568 Cross Reference: 47364
  • 1.5500 inches overall length
  • 1.1200 inches overall diameter
  • u/o f101-ge-102 engine, e/i b1-b end application
  • permanent magnet construction
1156M95P02 NSN 2925-01-194-9737 Cross Reference: 1156M95, 47479
  • 3.3500 inches overall length
  • 0.6100 inches overall diameter
  • u/o f-118 engine; e/i f16 c-d aircraft end application
  • permanent magnet construction
4057415 NSN 2925-01-206-7678 Cross Reference: 44839
  • 2.6900 inches overall length
  • 2.0500 inches overall diameter
  • u/o f100-pw-220 engine end application
9972258G1 NSN 2925-01-213-6622 Cross Reference: WW-5051763 PIECE 68
6437W10G703 NSN 2925-01-225-0673 Cross Reference: 6437W10G701
  • f101 engine fuel flow transmitter end application
2607926-800 NSN 2925-01-271-4635
4059985 NSN 2925-01-298-2674 Cross Reference: 46122
  • f100 engine end application
  • agav criticality code justification
1526M44P03 NSN 2925-01-309-3075
  • 3.350 inches overall length
  • ac current type
  • between 1.999 inches and 2.001 inches overall diameter
  • permanent magnet construction
  • rotor generator style designator
85661-1 NSN 2925-01-314-3823
9030D23-1 NSN 2925-01-314-5833
  • aircraft av-8 end application
30076-352 NSN 2925-01-314-9682
  • aircraft model h-1 end application
46038 NSN 2925-01-343-5844 Cross Reference: 1B4248
  • c-17 aircraft end application
1697M68G01 NSN 2925-01-355-3866
  • f110-ge-400 engine end application
  • heat sleeve to 500 degree fahrenheit special features
5873790-101 NSN 2925-01-355-5106
9334M40P03 NSN 2925-01-407-3032 Cross Reference: 47364-2
  • 1.550 inches overall length
  • ac current type
  • 2.315 inches overall diameter
  • f101-ge-102 engine end application
  • asdifferentiated by source control dwg reference number differentiating characteristics
1526M44P06 NSN 2925-01-421-9665 Cross Reference: 45867-1
  • f110/ge129 engine end application
  • rotor to mated with stator ge dwg1376m46 special features
  • as differentiated by source control dwg reference number differentiating characteristics
1B4891 NSN 2925-01-423-4962 Cross Reference: 46304
1526M44P05 NSN 2925-01-437-1128 Cross Reference: 1526M44, 46695-1
  • 3.350 inches overall length
  • between 1.981 inches and 1.989 inches overall diameter
  • f110/ge100 afct engine end application
  • rotor mated with stator ge drawing 1376m46p06 special features
  • as differentiated by source control drawing reference number differentiating characteristics
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