Air Turbine Engine Starters - Page 4 of 6

145 part numbers
383780-2-1 NSN 2995-01-173-7510
  • 8.400 inches major diameter
  • 3.636 inches outside diameter
  • u/o c135e, ec135e, kc135e acft end application
  • spline drive type
  • not included standard mounting feature
383222-4-1 NSN 2995-01-173-7511
  • 8.400 inches major diameter
  • 3.636 inches outside diameter
  • u/o c135e, ec135e, kc135e acft end application
  • spline drive type
  • not included standard mounting feature
383370-4-1 NSN 2995-01-173-7512
  • 3.631 inches outside diameter
  • u/o c135e, ec13e, kc135e acft end application
  • spline drive type
  • not included standard mounting feature
  • round flange shape
383370-3-1 NSN 2995-01-173-7513
  • 3.631 inches outside diameter
  • u/o c135e, ec135e, kc135e acft end application
  • spline drive type
  • not included standard mounting feature
  • round flange shape
354870-1 NSN 2995-01-173-7514
  • 8.320 inches major diameter
  • u/o c135e, ec135e, kc135e acft end application
  • spline drive type
  • not included standard mounting feature
  • round flange shape
354690 NSN 2995-01-174-0861
  • 8.320 inches major diameter
  • u/o c135e, ec135e, kc135e acft end application
  • spline drive type
  • not included standard mounting feature
  • round flange shape
355290-1 NSN 2995-01-174-0862
  • 8.320 inches major diameter
  • u/o c135e, ec135e, kc135e acft end application
  • spline drive type
  • not included standard mounting feature
  • round flange shape
383370-1-1 NSN 2995-01-174-0863
  • 3.631 inches outside diameter
  • u/o c135e, ec135e, kc135e acft end application
  • spline drive type
  • not included standard mounting feature
  • round flange shape
730795D NSN 2995-01-187-9818
  • 20 teeth quantity
  • spline drive type
  • not included standard mounting feature
  • round flange shape
  • 3.510 inches inlet flange mounting hole diameter
36E84-18QF NSN 2995-01-194-8153
  • 2 mounting hole quantity
  • u/o c130h aircraft end application
  • spline drive type
  • not included standard mounting feature
  • rectangular flange shape
3505412-5-1 NSN 2995-01-224-4882 Cross Reference: 10183260, 3505412-4-1
  • 51.6 pounds per square inch air supply inlet pressure
  • err default err default
3505674-1 NSN 2995-01-227-6649 Cross Reference: 3505230-4-1
  • c-130 acft end application
  • to.2ja3-56-4, fig.1.1 reference data and literature
3505672-1 NSN 2995-01-227-6650 Cross Reference: 3505228-2-1
  • c-130 acft end application
  • to. 2ja3-55-4 reference data and literature
36E162-2B NSN 2995-01-231-5063 Cross Reference: 36E162-2A
  • used on sentry f22 aircraft end application
7-116320000-5 NSN 2995-01-245-6008 Cross Reference: 3505300-4-2
  • counterclockwise drive rotation direction
  • any acceptable air inlet connection type
3505586-4-1 NSN 2995-01-255-6852 Cross Reference: 3505586-2, 3505586-3
  • 11.170 inches major diameter
  • pacer special, apu end application
  • 59364 document source
  • spline drive type
  • included standard mounting feature
MIL-S-19557/10 NSN 2995-01-256-8372
  • aircraft model fa-18 end application
  • 20 teeth quantity
  • spline drive type
  • included standard mounting feature
  • round flange shape
A55P9020-5 NSN 2995-01-277-8259 Cross Reference: 3505600-3-1
  • f-14 acft end application
53WK16012 NSN 2995-01-309-1925
  • ch-53e helicopters end application
3505354-1-2 NSN 2995-01-311-2334
36E80-12QC NSN 2995-01-316-0727 Cross Reference: MIL-S-19557
  • e-2c acft end application
  • parts kit, aircraft fsc application data
3505558-2-1 NSN 2995-01-316-0728
  • c2/e-2 acft end application
  • clockwise drive rotation direction
  • parts kit, aircraft fsc application data
3505710-2-1 NSN 2995-01-323-9808 Cross Reference: 17B8D8620-1, 3505710, ATS100-384P
  • c-17 aircraft, f117 engine end application
3502760-2 NSN 2995-01-324-2798
  • c-17 end application
36E165-2QC NSN 2995-01-329-6341
  • c-130 aircraft end application