Turbine max speed is 11rpm, that's a speed of 48.4 m/s at a radius of 42 m (where the A380's center of gravity should pass). At the same radius, the free space between two blades should be about 85-86 m. Subtracting the A380's fuselage height of 8.41 m, I get a possible passage time of 1.6 seconds. With the A380's length of 73.73 m, you'd need a speed of at least 165 km/h to pass. Even minimum takeoff speed (about 250 km/h) is above, so the A380 wins :-)

_{*Lunatic*, n.
One whose delusions are out of fashion.}