Engine Oil Pump Assemblies
92 part numbers
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tf41 engine end application
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8.50 gpm at 50.0 psig special features
9642M24P03
NSN 2995-00-102-7673
Cross Reference:
GM564-2
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9.330 inches overall length
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aircraft eng tf-39 end application
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agav criticality code justification
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diameter min. 4.747 and max. 4.749 special features
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tf41 engine model number for which designed
5008T68P07
NSN 2995-00-152-0883
Cross Reference:
GD321-10
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t-64 engine end application
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as differentiated by source control dwr no. reference number differentiating characteristics
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tf-39 engines end application
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agav criticality code justification
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found in t.o. 2j-tf39-4 special features
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j-69 aircraft engine end application
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agav criticality code justification
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found in t.o. 2j-j69-64 special features
512D893
NSN 2995-00-446-2811
Cross Reference:
512D893P1, RG16710A
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feat criticality code justification
700823-1
NSN 2995-00-502-2452
Cross Reference:
GD252-2
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engine, acft, turbojet, model j69t25 end application
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agav criticality code justification
700873
NSN 2995-00-544-0493
Cross Reference:
700823, GD252-1
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model j69 aircraft engine end application
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agav criticality code justification
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aircraft eng t56 end application
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agav criticality code justification
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found in t.o. 2j-t56-14 special features
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aircraft eng t-56 end application
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agav criticality code justification
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found in t.o. 2j-t56-14 special features
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aircraft eng j85 end application
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agav criticality code justification
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found in t.o. 2j-j85-44 special features
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pump2995-00-446-2811pl: j-79 eng end application
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pump2995004462811pl; j-79 eng end application
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acftgaircraft eng t-56 end application
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found in t.o. 2j-t56-14 special features
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aircraft eng t64 end application
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agav criticality code justification
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tf 41 jet engine end application
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aircraft eng f100 end application
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aircraft engine t-56 end application
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agav criticality code justification
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aircraft eng tf34 end application
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agav criticality code justification
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found in t.o. 2j-tf34-4 special features
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tf141 engine end application
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f-100-pw-200 engines end application
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oh-58d turbine engine end application