Abstract: A navigable craft that includes a fuselage with a tiltable section positioned behind a non-tiltable section opposite to a nose. A set of wing assemblies connected to the non-tiltable section of the fuselage. Each wing assembly includes an airfoil connected to the non-tiltable section of the fuselage at a first cross-sectional end of the airfoil and a non-tiltable propulsion generator connected to a second cross-sectional end of the airfoil opposite to the first cross-sectional end of the airfoil. The propulsion generator extends parallel and adjacent to the non-tiltable section of the fuselage, and one or more stabilizers connected to at least one of the non-tiltable propulsion generator, the airfoil, and the fuselage. The landing assembly is connected to the propulsion generator or the airfoil. The landing assembly is aligned aerodynamically with the second cross-sectional end and extends in a direction adjacent to the tiltable section of the fuselage.