Turbine E Exhaust Nozzle Controls

8 part numbers
167352-2 NSN 2995-00-475-0698
  • u/o j-85 engine end application
  • t.o. 2j-j85-74 reference data and literature
512D715P13 NSN 2995-00-702-2471 Cross Reference: 535E396G11
  • engine, j79 end application
  • 13.261 in. lg, 10.422 in. w, 3.777 in. h general description
512D728G3 NSN 2995-00-735-2250
  • engine, jet, acft, j79 end application
512D715P10 NSN 2995-00-925-0445 Cross Reference: 512D715P3A, 512D715P8, 535E396G6, 535E396G8
  • j79-ge-15 aircraft engine end application
  • feat criticality code justification
  • fscap special features
  • aircraft engine fuel system components fsc application data
131D5023G02 NSN 2995-01-138-2303 Cross Reference: 37D401335P110
  • j85-ge-5/-13 aircraft engine end application
441612 NSN 2995-01-319-5004 Cross Reference: 4076322
  • f100-pw-229 end application
  • aluminum alloy material
  • t.o.2j-f100-54, f.48 reference data and literature
4083219 NSN 2995-01-433-6462 Cross Reference: 441944, 441944-10, 441944-ISS10
  • f100-pw-129 aircraft engine end application
  • agav criticality code justification
  • as differentiated by source control drawing reference number differentiating characteristics
2663917 Convergent Control-exhaust Nozzle NSN 2995-01-450-2816 Cross Reference: 4083931, 441991-11
  • 11.000 inches overall height
  • 5.000 inches overall width
  • f100-pw-220 aircraft eng end application
  • t.o. 6j3-8-21-4 reference data and literature
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