STORM VANTAGE Powered By Rotax or Lycoming engines

Contact: atrstormgroup@gmail.com

Price: 83.500 Euro LSA Standard version - Crating 500 - 5 years Warranty

The

Storm Vantage SLSAis an all-metal lowwing rcraft. Cutting edge aerodynamic design technology enables all of the aircrafts outside surfaces to generate life, thereby, addingmeasurably to the performance, stability, and fuel efficiency of this sleek new entry in the US SLSA market.

The Storm Vantage SLSAis available in tricycle or conventional landing gear. The wide cockpit area allows for ample room for the pilot, passenger and baggage. The highly developed canopy design provides outstanding visibility for pilot and passenger. The aircrafts large fuel tanks, and advanced low flight drag design give the aircraft exceptional cruising distance.

Longer than other Storm models (12 inches more than Storm Century), the fuselage of Storm Vantage consists of two basic sections: the first section includes landing gear beam, wing beam and cabin section, and the sheet-metal tail cone section.

State of the art Italian design!

Storm designed aircraft, with over 30 years experience in the aviation business

All metal constructed airframe. Available in taildragger or conventional landing gear

Nose wheel steering via rudder peddles

Pilot and co-pilot operated differential hydraulic disk toe brakes

Roomier interior; two 6 ft. plus size people sitting comfortably in a cockpit - 43.3 inches wide Large oversized one-hundred pound capacity luggage compartment.

Over 300 + degrees of visibility from adjustable seats using four point harness restraints

Complete interior paneling throughout with carpeted decks for a fully finished cockpit area

Cockpit heating and air ventilation. Secure key door locks with fore and aft stainless steel locking pins

Very stylish molded instrument panel superbly designed to easily relate vital pilot information

Electric elevator trim activated by multi-function control grips with panel indicator lights

Electric fowler flaps. Automatic push button operation to four preset settings with manual over-ride

All cabling and wiring fully enclosed, flight controls operated via push rods and stainless steel cables

High strength aluminum leaf landing gear legs to arrest aggressive landings

Uncompromised fit and finish using high quality epoxy coating materials for extended attractive life

Uses the defacto engine standard. The Rotax 100 hp. 912S and 3 blade carbon fiber manual adj. prop

Low fuel burn and low maintenance cost and upkeep encourages maximum utilization

Possibly the best product warrantees you will find for a Light Sport Aircraft

Manufactured to or beyond the ASTM standards established for Light Sport Aircraft

The Storm Vantage SLSAcan be used for VFR night flight and/or IFR flight operations (provided the individual aircraft is equipped with the required FAA-Federal Aviation Administration certified equipment for these operations).This aircraft offers exceptional performance,stability, pleasure, economy and safety to the sport pilot.. but also provides all other certificated airment 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!

The empennage (tail) of the new Strom Vantage demonstrates the design and construction efficiency of Storm Aircraft. The tail is comprised of a single horizontal tail (stabilator) and a single vertical tail (rudder). The stabilator is dynamically balanced and mounted to the fuselage with two large steel bearings. Operation of the stabilator is through the push-pull movement of the control wheel yoke control. The "flying tail" stabilator is equipped with dual trim tabs (interconnected) mounted on the trailing edge. The trim tab is actuated by an electric trim motor, which is activated by the pilot by moving a electric trim wheel, similar to conventional aircraft.

STORM VANTAGE Engines 100 to 180 hp

Seats	2 Seats		Experimental 2 + 2
Cabin Widht	1,12 mt
Length	7,20 mt
Wing Span	8,60 mt
Wing Area	11,098 m2
Empty Weight	290 kg		410 kg
MTOW	600 kg	750 kg	750 kg
Capacity Usuable Fuel ( 100 lt - 160 lt Long Range tanks)
Range 75% of Power	1600 - 2580 km		1300 - 2000 km
Takeoff Distance	125 mt		180 mt
Landing Distance	160 mt		210 mt
Climb Rate	1000 ft/m		1200 ft/m
Vs.	63 km/h		68 km/h
Vso.	72 km/h		78 km/h
V max.	248 km/h		290 km/h
Vcr @ 75% of Power	220 km/h		275 km/h
Vne.	320 kmh		320 km/h
Engine Rotax 100 to 140 hp - Lycoming	100 hp		160 hp