A 40% increase in aileron surface area, together with a refined airflow design aided by vortex generators, allow the pilot to keep full control authority at extremely low speed on approach. Shock’s Fowler flaps extend 70% from their retracted area and the flaps can be equipped with mini vortex generators installed inside the vane (see video). Zlin and SportairUSA love VGs; they are available for the wings, rudder, flaps and horizontal tail.
The significant increase in wing lift provides added performance in landing and takeoff. With the 180-horsepower Titan engine doing the pulling, Outback Shock can launch in less than 200 feet at gross weight and land in barely over 100 feet. With a single occupant these numbers are halved.
One part of the takeoff and landing prowess of Shock is low stall speeds… really low.
Stall in the airplane with a single occupant is an astonishing 18 mph or about 15.6 knots; even at gross weight stall occurs at 23 mph (20 knots).
However, Outback Shock is not a particularly speedy cross country cruiser. “Max” speed is 115 mph or 100 knots. Typical cruise is about 90 mph or around 80 knots.