Air Turbine Engine Starters
145 part numbers
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aircraft model p-3b end application
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any acceptable drive type
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not included standard mounting feature
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any acceptable air inlet connection type
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not included quick detachable mounting feature
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aircraft model e-2b end application
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any acceptable drive type
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not included standard mounting feature
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any acceptable air inlet connection type
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not included quick detachable mounting feature
36E81-6B
NSN 2995-00-038-1172
Cross Reference:
12SCP403-39, 36E81-6QB
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spline drive type
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flange air inlet connection type
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round shape
A-24-1
NSN 2995-00-045-3347
Cross Reference:
383650-1-1, 383650-12
383084-3-1
NSN 2995-00-051-2983
Cross Reference:
ATS100-176A
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aircraft model e-2b end application
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any acceptable drive type
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not included standard mounting feature
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any acceptable air inlet connection type
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not included quick detachable mounting feature
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aircraft model p-3b end application
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any acceptable drive type
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not included standard mounting feature
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any acceptable air inlet connection type
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not included quick detachable mounting feature
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99237 document source
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and20002 document identification
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included standard mounting feature
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45.0 pounds per square inch air supply inlet pressure
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450.0 degrees fahrenheit air supply inlet tempurature rating
36E123-2A
NSN 2995-00-078-2916
Cross Reference:
A29
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spline drive type
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round flange shape
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flange air inlet connection type
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1 quantity
36E79-12B
NSN 2995-00-111-3651
Cross Reference:
36E79-12QB
383652-1-1
NSN 2995-00-111-3653
Cross Reference:
383653-1
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aircraft model c2/e2 (common) end application
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any acceptable drive type
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not included standard mounting feature
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clockwise drive rotation direction
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any acceptable air inlet connection type
53WK16011
NSN 2995-00-122-9508
Cross Reference:
938097
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ch-53-e helicopters end application
MIL-S-19557C
NSN 2995-00-140-6832
Cross Reference:
3505128-1-1, ATS100-395
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between 3.272 inches and 3.292 inches outside diameter
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spline drive type
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counterclockwise drive rotation direction
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flange air inlet connection type
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not included quick detachable mounting feature
36E81-6A
NSN 2995-00-169-0025
Cross Reference:
1128SCP403-15
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not included quick detachable mounting feature
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engine aircraft fsc application data
36E118-2A
NSN 2995-00-178-0895
Cross Reference:
36E118-2B
737079
NSN 2995-00-199-0983
Cross Reference:
737079-1
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aircraft model a-4 end application
715960-1
NSN 2995-00-251-7098
Cross Reference:
PS400-36
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and20002 document identification
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included standard mounting feature
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70.0 pounds per square inch air supply inlet pressure
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218.3 degrees celsius air supply inlet tempurature rating
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110.0 pounds per minute air supply flow rate
36E118-2D
NSN 2995-00-304-8183
Cross Reference:
MIL-S-22518
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99551 document source
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36e118&2d document identification
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spline drive type
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included standard mounting feature
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not included quick detachable mounting feature
SKP36130
NSN 2995-00-337-5116
Cross Reference:
3505230-1-1, ATS100-422
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1.264 inches major diameter
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3.190 inches outside diameter
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1.090 inches minor diameter
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99237 document source
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and20002 document identification
SKP36129
NSN 2995-00-337-5145
Cross Reference:
3505228-1-1, ATS100-421
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1.264 inches major diameter
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3.190 inches outside diameter
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1.090 inches minor diameter
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99237 document source
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and20002 document identification
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clockwise drive rotation direction
36E83-8A
NSN 2995-00-419-6293
Cross Reference:
36E86-6A
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aircraft model a-4 end application
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agav criticality code justification