
            
            
            
            With over 10 years in 
            aircraft industry S.G.Aviation has become one of the most successful 
            kit and ready to fly manufacturers in the world in its category. S.G. 
            Aviation manufactures the world’s finest Made in Italy style 
            aircrafts with a proven builder assistance program, flight training 
            and dedicated technical support, S.G.Aviation assures builders’ 
            success in building and safety flying these aircrafts in a short 
            time. 
            
            The Storm 400 offers superior performance and 
            capabilities for a 2+2 place, comfortable side-by-side seating, 
            improved cabin space, and best of all, the Storm 400 is available on 
            kit and ready to fly as other Storm models. The Storm 400 is easy to 
            build, easy to fly, true high performance airplane with the ability 
            to make long cross country trips. No other aircraft offers the 
            quality, performance, comfort and superior design of the standard 
            Storm 400. Longer 4 inches more than Storm 280 and 300 series, the 
            Storm 400 has large space area improved both inside and outside. 
            
            The 
            all sheet metal fuselage is a conventional semi-monocoque structure: 
            a basic rectangular section formed by four longerons, with skins 
            blind riveted to the longerons (and stiffeners). Fuselage structure 
            is a all-metal framework for cabin area high protection and semimonococque light alloy tail to support empennage. Easy to 
            inspect, the Storm 400 has immediate access’ for servicing to be 
            efficient and inexpensive at the same time.
            
            The Storm 400 is a 2+2 place with improved cabin space than 280 and 
            300 series. The cabin width is an amazing 43 inches from window to 
            window. The wide cabin (1,10 m) features two side by side seats 
            adjustable via sliding rail stops, and a large space behind forward 
            seats that can be occupied by 2 passengers or by baggage.
            
            The wide windshield offers a complete view unhindered by structural 
            elements, while large side windows allow for excellent visibility.
            
            The entirely moving tailplane permits superior control and a high 
            degree of stick free stability, moving surfaces feature mass 
            balancing. 
            
            The wing is of all-metal stressed-skin full-cantilever low-wing 
            design consisting of two wing panels bolted to a spar box assembly 
            in the fuselage. The wing has a high lift airfoil and wing tips to 
            maximize effective wing span. The electrically activated flaps, 
            allow stall speeds under 38Kts. With flaps deployed, a steep 
            approach is possible resulting in a very short landing distance.
            The Storm 400 utilizes the same gear system of other Storm models, 
            developed specifically for flight training operations. The main gear 
            is a 2 aluminium springs that provide double cantilever deflection. 
            Four large bolts for each side hold up the 2 springs to a fuselage 
            beam inside. 
            
            It provides excellent grass-field capability, and is very durable, 
            simple and virtually maintenance-free. The nosewheel strut in the 
            three-gear version uses a single heavy-duty bungee for shock 
            absorbency. The nosewheel is steering, with direct linkage to the 
            rudder pedals for very effective and responsive ground handling and 
            tight turns. The main wheels are equipped with hydraulic disk 
            brakes. 
            
            Specially studied wheel fairings are mounted on each wheel to reduce 
            parasite drag. Engine cowling is made up two parts and allows for 
            quick and complete opening. Fuel tanks are integral part of the wing 
            structure and feature 65 litre capacity per each half wing. 
            Instrument panel meets General Aviation standards both in size and 
            quality allowing for installation of a wide variety of flight 
            instrumentation, engine controls and com/nav apparatus.
            Flight controls are traditional type with dual stick, dual rudder 
            pedals and dual throttle knobs on dashboard. Longitudinal trim and 
            electrical flap controls with position indicators are also located 
            on dashboard.
            Cabin ventilation is adjustable air vents fed via buried scoops.
            
             
              
               
               
               specifications 
 
              
                
                powerplant 
                propeller 
                length 
                height 
                wing span 
                wing area 
                seats 
                empty weight 
                
                useful load 
                gross weight 
                fuel capacity 
                range | 
                
                      Lycoming 
                      O320 160HP 
                x 
                
                      22,4 ft. 
                
                x 
                
                      26,2 ft. 
                
                      112,5 sq.ft. 
                
                      2 + 2 
                
                      1055 lbs 
                x 
                
                      1870 lbs 
                
                      37 gal. 
                
                      680 s.m. | 
               
             
            
            performance 
            
             
            
              
                
                takeoff distance, 
                ground roll 
                rate of climb 
                max speed 
                cruise speed 
                landing distance, ground roll 
                
                
                service ceiling | 
                
                      720 ft. 
                
                x 
                
                      180 mph 
                
                      170 mph 
                
                      655 ft. 
                x | 
               
             
            
            limiting and recommended speeds
             
            
              
                
                design manoeuvring speed (Va) 
                never exceed speed (Vne) 
                stall, power off (Vsl) 
                landing approach speed  | 
                
                
                x 
                
                      192 mph 
                
                      44 mph 
                x | 
               
             
            All specifications are based on manufacturer's 
            calculations 
   |