RALLY Aircraft   Contact: atrstormgroup@gmail.com

State of the art design!              TheStorm Rally is the latest in state of the art  Special Light Sport Aircraft design. The Rally is a result of many years of extensive research and development; carbon fiber and Kevlar are utilized in the constructionof the Rally to create a lightweight and extremely strong airplane. Its composite structure is not subject to rot, rust or corrosion.          This design increases performance and helps to reduce maintenance and repair costs. This SLSA aircraft has the largest overall cabin in its category/ class/set available on the market today. The well designed and placed windows provide over 300 degrees of visibility for the pilot and passenger. Its unique gull type door design allows for easy entry and exit by pilots or passengers over 6’2 tall! These doors can be opened in flight at speeds of 60 knots or less for incredible photo and/or video taking opportunities.            The aircraft is forgiving, quick, responsive and precise to the pilot’s touch. The Rally SLSA has exceptional natural Short Take off and Landing (STOL) performance characteristics do to its extraordinary aerodynamic design and can be used for Visual Flight Rule (VFR) night flight and/or (IFR) Instrument Flight Rule flight operations (provided the individual aircraft is equipped with the required FAA-Federal Aviation Administration certified equipment for these operations).           This aircraft offers exceptional high-wing performance, pleasure, economy and safety to the sport pilot ... but also provides all other certificated airmen new opportunities for affordable personal aircraft ownership and air travel. Get above the traffic jams and highway stress with an aircraft that will get you there and back for  less than half the fuel and time that an automobile can!               RALLY SPECIFICATION     Exterior Dimensions   Span .......................................................................    30 ft 1 in   Length......................................................................    23.2 ft   Height......................................................................      7 ft   Wing Area................................................................  124.96 sq ft   Interior Dimensions   Cabin Height (top of seats to roof)................................    40 in   Cabin Width (door to door, at the handle) .....................    43.7 in   Cabin Length (instrument panel to rear bulkhead) .........    70 in   Baggage Space.........................................................    16 cubic ft   Powerplant/Systems   Model.......................................................................     Rotax 912 UL S2   Power/rpm................................................................     100 hp / 5800 rpm   Propeller   Type .......................................................................      3 blades ground adjustable   Diameter .................................................................      70 inches       PERFORMANCES CHART   Speed   Maximum at sea level...................................................................    120 knots   Cruise (75% power at 2000 ft, ISA conditions) ...........................    107 knots   34 Gal Usable Fuel   ..............................................................   Time 7.2 hours   Cruise   75% at 2000 ft (ISA conditions)...................................................   Range 800 Nm   Rate of climb at sea level..........................................................   800 ftm   Service ceiling............................................................................  12000 ft   Takeoff Performance - (ISA Conditions - Sea Level).   Ground roll .....................................................................................  360 ft   Total Distance over 50 ft obstacle...............................................    600 ft   Landing Performance - (ISA Conditions - Sea Level)   Ground roll ...................................................................................    450 ft   Total Distance over 50 ft obstacle............................. ..................  1000ft   Stall Speed   Flaps up, power off..................................................................      44 knots   Flaps down, power off..............................................................     35 knots   Maximum Weight   Light Sport Aircraft rules ...........................................................   1320 lbs   Standard Empy Weight   Light Sport Aircraft.....................................................................  760 lbs    Maximum Useful Load   Light Sport Aircraft..................................................................... ..  560 lbs .. Wing Loading                                                                                        Light Sport Aircraft...................................................................  10.34 lbs/sq ft   Power Loading.......................................................................   13.2 lbs/hp   Total Fuel Capacity   Standard Wing Tanks..............................................................   35 gal/34 usable   Oil Capacity ...........................................................................   0.8 gal                                            A.T.R     Aero Technology  & Research     atrstormgroup@gmail.com   Join Us on:           info@stormaircraft.com   tech@stormaircraft.com About Us Why Storm Aircraft CAD & Stress Analysis Aerodynamics Media Dealers Aircraft Model  RG FURY RALLY CENTURY VANTAGE FURY AGRI SEASTORM Africa Brand contact contact@avionav.net                                                                                                                                                                          Coming soon