Th
|
![]() |
![]() |
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
![]() |
![]() |
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.
|
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 |
Engines |
Rotax 915 - 141 hp |
Lycoming IO 360 - 160 hp |
![]() |
![]() |
Rotax 9120 IS - 100 hp |
Lycoming 233 S - 115 hp |
![]() |
![]() |
Copyright & S All rights reserved.
This website was powered by Ewisoft Website Builder.
|