2-person ULM aircraft Savannah™ ADV

4-stroke enginetouristsingle-engine

The Savannah™ ADV was born from the idea to join together in a sole aircraft the possibility to make extremely short landing and have high cruising speed. The system, fully planned and produced by I.C.P., permits through the activation of a button, the leaking out of generous high-lift from the wing profile. These are interlocked to avoid the leak out from only one side. Certified LSA in the United States and in Australia, this aircraft is planned for a maximum takeoff weight of 560 Kilograms. It is sold with engine Rotax 912S (100hp), electric variable pith prop, lights of navigation and strofe on the wings, fairing wheels, trim with electric control on the elevator and led indicator of position, intercom, 2 headphones, radio predisposition and others accessories. StructureClick to show – The Savannah™ ADV is a monoplane type, with two side-by-side seats, fitted with a high wing supported by struts. – The wings are trapezoidal with aerodynamic profile NACA 23015, provided with twist and dihedral and its lift system consists of slats on the leading edge and double-slot flap on the trailing one. – The slats slide on 4 ways operated by the same amount of levers, which are handled by a torque tube. – The horizontal empennage is tapered and it consist of a fixed stabilizer and a moving balancer. Both the fixed part and the moving one are carried out in two half planes. The left balancer is provided with trim wing and motor located in the front housing of the elevator with position indicator. CockpitClick to show – The two large lateral doors allow an easy independent access to the cabin.