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. . <br /> ICGeminus Boeing Project Contract No.EVE-16-2929 <br /> Technology Development CEI Project No. 160731 <br /> aft fuselage stacker (and paint gun) was moved forward slightly to make room for the high bay <br /> stacker position. <br /> s <br /> /• fit...-_i y '_ ^?"=s`3 <br /> rit <br /> .� •.�� - <br /> r�,1j!� r <br /> s <br /> TA: it <br /> 1' <br /> ..4444ioliiiitivior. , <br /> Figure 84: Location of the high bay stacker during all Case 3 scenarios. High bay <br /> stacker located so that painter can exit onto the HSP configured for painting <br /> bottom of the horizontal stabilizer. HSP raised up to 2' below HS bottom <br /> surface for Case 3/Scenario 2b. <br /> Figure 85 depicts the locations and orientations of the spray guns used in this simulation. <br /> Figure 86 through Figure 88 depicts the size of the >2% LEL volumes around the aircraft. <br /> II <br /> Figure 89 depicts the % of LEL levels at the entrances of the floor exhausts. Figure 90 through <br /> Figure 98 show contour x-sections of% of LEL for Case 3/Scenario 2b on the aircraft centerline <br /> and on cut planes defined in Figure 59. <br /> 80 <br />