Building away on the -8A fuselage and notice that on the drawing side view, the "line" for the nosewheel is lower than the mains, making me think the fuselage is intended to not be level, but pointing upwards somewhat on the ground...
Just curious if this is common with other "A" models and what the reason might be- prop clearance, handling characteristics, etc.? Would this incidence make the airplane more robust in some way?
Just curious if this is common with other "A" models and what the reason might be- prop clearance, handling characteristics, etc.? Would this incidence make the airplane more robust in some way?