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The Rotax 503 is a 37 kW (50 hp), inline 2-cylinder, two-stroke aircraft engine, built by BRP-Rotax GmbH & Co. KG of Austria for use in ultralight aircraft. [ 1 ] [ 2 ] For decades the engine was one of the most popular and reputedly reliable aircraft engines in its class (two-stroke, under 60 horsepower), [ 3 ] and it remains widely used and ...
The initial engine recommended for the design was the now out-of-production 28 hp (21 kW) Rotax 277. Recommended engines today include 40 hp (30 kW) Rotax 447 and the 50 hp (37 kW) Rotax 503 . Kit options include brakes, an extra 5 US gal (19 L) fuel tank, spoked wheels, floats and skis.
Print/export Download as PDF; Printable version; In other projects Wikimedia Commons; ... Rotax 503; Rotax 532; Rotax 535; Rotax 582; Rotax 618; Rotax 912; Rotax 914 ...
Standard engine was the Rotax 447 of 40 hp (30 kW), with the Rotax 503 of 50 hp (37 kW) and the Rotax 582 of 64 hp (48 kW) optional. Reported construction time 200 man-hours including complete cockpit fairing. Empty weight of 390 lb (177 kg) places the S-14 above the maximum category weight of the US FAR 103 Ultralight Vehicles category ...
Two-seat variant powered by a 115 hp (86 kW) Rotax 914, 115 hp (86 kW) Subaru EA-81 automotive conversion, or similar engine. Four flying by 1998. [2] [3] Rotor Flight Dynamics Dominator UltraWhite A lightweight version of the Dominator without any fairing and powered by a 50 hp (37 kW) Rotax 503 two-stroke. [4] Rotor Flight Dynamics Dominator ...
The standard engine supplied was the twin cylinder, liquid-cooled, two-stroke, dual-ignition 64 hp (48 kW) Rotax 582 engine in pusher configuration. The 50 hp (37 kW) Rotax 503 and 40 hp (30 kW) Rotax 447 engines were factory options. [1] The aircraft fuselage is made from metal tubing, while the fairing is fiberglass. Its two-bladed rotor has ...
The original basic engine was the Rotax 277 of 28 hp (21 kW), with the Rotax 447 of 40 hp (30 kW) and the Rotax 503 of 50 hp (37 kW) available later as options. [ 1 ] [ 2 ] [ 11 ] The Coyote II two-seater was later developed from the S-5.
The basic engine is the Rotax 503 of 50 hp (37 kW), with the Rotax 582 of 64 hp (48 kW) and the Hirth 3701 of 100 hp (75 kW) available as options. [ 1 ] [ 2 ] [ 10 ] The S-10 Sakota aerobatic two-seater was later developed from the S-9.