RALLY Aircraft

State of the art design!
The Storm 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 construction of 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

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