Eclipse

ECLIPSE is a very modern progressive conception, developed under recent knowledge of aerodynamics and hi-tech construction: a single-engine side-by-side all-composite high-wing two-seater with a fixed tricycle landing gear (a steerable nose wheel included). The aircraft design and construction is determined to recreational flying as well as flight training. Provided by a sufficient level of aircraft equipment any realization of long distance cross-country flights are also possible. Those aspects are emphasized by easy manoeuverability and comfortable cockpit space with a roomy baggage compartment (up to 32 kg) behind the seats.

It's spacious cabin with a 1,20 m width at shoulders not restricting your sitting comfort. It's excellent flight output provided with a precise and responsive control system, it's aircraft stability, great flight parameters such as brave climb rate, economical cruise speed, max. horizontal speed as well as low operating cost make the ECLIPSE safe, handy-sized, powerful and economic.

Smartly designed and optimized aircraft dimensions and specifications allow, besides above described parameters, also operations from unpaved airstrips. Aerodynamical construction ensures the highest possible performance and enables a choice of your favoured options with our focus on keeping the maximal custom-built quality.

Aircraft Details	UL (Ultralight)	LSA (Standard)

Empty Weight	285 kg	300 kg
MTOW	472,5 kg	600 kg
Wing Span	9,71 m	9,71 m
Length	6,34 m	6,34 m
Height	2,18 m	2,18 m
Wing Area	11,50 qm	11,50 qm
Engine, 4 cylinder, 4 stroke	Rotax 912 UL	Rotax 912 ULS
Power	80 Hp	100 Hp
Fuel capacity	130 ltr.	130 ltr.
Fuel consumption	14 l/h	16 l/h
Range	1.300 km	1.000 km
Endurance	9 hrs.	8 hrs.
Stall Speed (Vmin)	65 km	65 km
Optimum Speed (Vopt)	200 km	220 km
Max. Speed (Vne)	280 km	280 km