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In 2009 the standard recommended engine was the Rotax 447, with the 46 hp (34 kW) Rotax 503 single carburettor engine optional. [ 6 ] [ 12 ] In 2021 an electric aircraft option was added as the manufacturer offered a complete electric drivetrain and up to four batteries as an alternative to gasoline powerplants.
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 ...
Version with the Mild wing and Rotax 582 engine of 64 hp (48 kW) and dual floats for water operations. [3] XP-12 Buggy 582 SL Version with the XP-12 wing and Rotax 582 engine of 64 hp (48 kW) and float for water operations. [2] [3] MILD-GTE 503 SL Version with the MILD wing of 178 sq ft (16.5 m 2) and Rotax 503 engine of 50 hp (37 kW) [4] MILD ...
It was powered by a German Sachs SA-340 direct drive engine with a 336 cc displacement. This model sold for USD$2,850 in 1980. [6] Pfledge 430D The Pfledge 430D was announced late in 1979. This model featured a Cuyuna 430D engine which McCornack helped design. The engine was a two cylinder, two stroke engine with a displacement of 429 cc and a ...
The Firestar was intended to be a FAR 103 legal ultralight when powered by the 28 hp (21 kW) Rotax 277 engine. The 40 hp (30 kW) Rotax 447 or the 50 hp (37 kW) Rotax 503 were optional engines, although the aircraft then falls into the US Experimental - amateur-built category.
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The Nimbus engines were produced in two main variants, the Mark 103/503 and the Mark 105/502. The Mark 103/503 is generally similar to the Mark 105/502 except that the former has a double-caliper disc brake incorporated in the output drive shaft to provide adequate braking of the helicopter's rotor in the high winds encountered over the deck of a fast moving ship, whereas the 105/502 has a ...
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 ...