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Gemnus Boeing Project Contract No.EVE-16-2929 <br /> Technologyi Development CEI Project No. 160731 <br /> otip <br /> • <br /> 410.e. -`i•' w 1. A,• '+ �^ <br /> 60°S.°°°400101011111C -ft°°1001°°-- <br /> .40111111111111111111111. <br /> ./ r <br /> 1►. • j t �•� <br /> NVO 000t, <br /> Figure 9: Case 1/Scenario 1 (top) and /Scenario 2 (bottom) 45-04 Hanger Components <br /> Configuration. <br /> The general 45-04 interior configuration consisting of the aircraft, wing stands, tail & <br /> empennage stands and stacker cranes for Case 2 is shown in Figure 10. Note that the engine <br /> insert storage stand has been eliminated as this is being placed in the low-bay section of the 45- <br /> 04 hangar (similar to the 45-03). The interior configuration of Case 1/Scenario 2 is similar to <br /> that of Case 2/Case 3 Scenarios with the differences being primarily in detailed design of the <br /> new wing/tail/empennage stands, stacker details, and location of the stackers during wing & HS <br /> painting operations. Both Case 2 and Case 3 configurations were approved by Boeing for CFD <br /> analysis during the various weekly/bi-weekly meetings. <br /> 17 <br />