FIG. 1 is a top perspective view of a first aircraft fuselage, wherein wings are shown as these may be attached to the aircraft fuselage;
FIG. 2 is a bottom perspective view of the aircraft fuselage, wherein wings are shown as these may be attached to the aircraft fuselage;
FIG. 3 is a top perspective view of the aircraft fuselage;
FIG. 4 is a top view of the design corresponding to FIG. 1;
FIG. 5 is a bottom view of the design corresponding to FIG. 2;
FIG. 6 is a front view of the design corresponding to FIG. 1;
FIG. 7 is a back view of the design corresponding to FIG. 1;
FIG. 8 is a right side view of the design corresponding to FIG. 1;
FIG. 9 is a left side view of the design corresponding to FIG. 1;
FIG. 10 is a top perspective view of a second aircraft fuselage, wherein wings are shown as these may be attached to the aircraft fuselage;
FIG. 11 is a bottom perspective view of the second aircraft fuselage, wherein wings are shown as these may be attached to the aircraft fuselage;
FIG. 12 is a top perspective view of the second aircraft fuselage;
FIG. 13 is a top view of the design corresponding to FIG. 10;
FIG. 14 is a bottom view of the design corresponding to FIG. 11;
FIG. 15 is a front view of the design corresponding to FIG. 10;
FIG. 16 is a back view of the design corresponding to FIG. 10;
FIG. 17 is a right side view of the design corresponding to FIG. 10; and,
FIG. 18 is a left side view of the design corresponding to FIG. 10 and wherein the wings are shown in broken lines and do not form a part of the design.