"},"type":{"wt":"Twin-cylinder, two-stroke aircraft engine"},"bore":{"wt":"{{convert|69.5|mm|in|2|abbr=on}}"},"stroke":{"wt":"{{convert|60.0|mm|in|2|abbr=on}}"},"displacement":{"wt":"455 cc (27.77 cu in)"},"length":{"wt":"{{convert|14.5|in|mm|2|abbr=on}}"},"diameter":{"wt":""},"width":{"wt":"{{convert|16.0|in|mm|2|abbr=on}}"},"height":{"wt":"{{convert|16.0|in|mm|2|abbr=on}}"},"weight":{"wt":"{{convert|59|lb|kg|0|abbr=on}}"},"valvetrain":{"wt":"piston porting"},"supercharger":{"wt":""},"turbocharger":{"wt":""},"fuelsystem":{"wt":""},"fueltype":{"wt":"Minimum 92 octane"},"oilsystem":{"wt":"premixed oil and fuel"},"coolingsystem":{"wt":"fan cooled"},"power":{"wt":"{{convert|35|hp|kW|0|abbr=on}} at 6000 rpm"},"specpower":{"wt":""},"compression":{"wt":""},"fuelcon":{"wt":""},"specfuelcon":{"wt":""},"oilcon":{"wt":""},"power/weight":{"wt":""},"designer":{"wt":""},"reduction_gear":{"wt":"cog belt or optional gearbox"},"general_other":{"wt":""},"components_other":{"wt":""},"performance_other":{"wt":""}},"i":0}},"\n\n"]}" id="mwYg">
Data from Cliche [1]
The MA is a straight-4 SOHC 0.9 L, 1.0 L, or 1.2 L engine first introduced in 1982 by Nissan, intended primarily for the K10 series Micra/March model. It shares design similarities with the older E engine, with an 8-valve hemispherical cylinder head but differs in that it uses an aluminium cylinder block. Unusually, the specified ignition timing for the MA10 running on the specified 90 RON gasoline was 2 degrees after top dead centre, reflecting a very high flame speed in the compact combustion chambers.
The Lycoming GSO-580 is a family of eight-cylinder horizontally opposed, supercharged, carburetor-equipped aircraft engines for both airplanes and helicopters, manufactured by Lycoming Engines in the late 1950s and early 1960s.
The Lycoming O-340 is a family of four-cylinder horizontally opposed, carburetor-equipped aircraft engines, that was manufactured by Lycoming Engines in the mid-1950s.
The E0 series is a three-cylinder gasoline engine developed and manufactured by Honda, with a total displacement of 656 cc. The engine is intended for kei car applications. The E05A and E07A were partially replaced by the Honda P engine but as of 2020 the E07Z engine still saw use in the Acty truck.
The Cuyuna 430 and Cuyuna 340 are a family of two-stroke, twin-cylinder piston snowmobile engines that were redesigned to serve as ultralight aircraft powerplants.
The Hirth F-33 is a single cylinder, two stroke, carburetted aircraft engine designed for use on ultralight aircraft, including powered paragliders and ultralight trikes. the engine is noted for its extremely light base weight of 35 lb (16 kg). It is manufactured by Hirth of Germany.
The Hirth 2704 and 2706 are a family of in-line twin cylinder, two stroke, carburetted aircraft engines, with optional fuel injection, designed for use on ultralight aircraft and especially two seat ultralight trainers, single seat gyrocopters and small homebuilts. It was manufactured by Hirth of Germany.
The Hirth F-30 is a horizontally opposed four-cylinder, two-stroke, carburetted aircraft engine, with optional fuel injection, designed for use on ultralight aircraft and homebuilts. It is manufactured by Hirth of Germany.
The Hirth 3701 is an in-line three-cylinder, two-stroke, carburetted aircraft engine, with optional fuel injection, designed for use on ultralight aircraft and small homebuilts. It is manufactured by Hirth of Germany.
The Hirth F-36 is a single-cylinder, two-stroke, carburetted aircraft engine designed for use on ultralight aircraft, especially powered paragliders and ultralight trikes. It is noted for its extremely small equipped weight of 28 lb (13 kg) including exhaust system, reduction drive and carburetor. It is manufactured by Hirth of Germany.
The Hirth 3202 and 3203 are a family of in-line twin cylinder, two stroke, carburetted aircraft engines, with optional fuel injection, designed for use on ultralight aircraft, especially two seat ultralight trainers, gyrocopters and small homebuilts. It is manufactured by Hirth of Germany.
The Hirth 3502 and 3503 are a family of liquid-cooled, in-line twin-cylinder, two-stroke, carbureted aircraft engines, with optional fuel injection, designed for use on ultralight aircraft and small homebuilts. It is manufactured by Hirth of Germany.
The 2si 230 is a family of single-cylinder, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft.
The 2si 540 and 2si 500 are a family of in-line twin-cylinder, liquid-cooled, two-stroke, dual ignition, aircraft engines that were designed for ultralight aircraft.
The 2si 215 is a family of single-cylinder, fan-cooled, two-stroke, single ignition, aircraft engines that were designed for ultralight aircraft.
The 2si 690 is a family of in-line three cylinder, liquid-cooled, two-stroke, dual ignition, aircraft engines that were designed for ultralight aircraft.
The 2si 808 is a family of in-line three cylinder, liquid-cooled, two-stroke, dual ignition, aircraft engines that were designed for ultralight aircraft.
The Arrow 250 is a family of single-cylinder, two-stroke, single- or dual-ignition aircraft engines that were designed for ultralight aircraft by Arrow SNC of Italy.
The Fletcher Hercules is an American two-seat ultralight trike that was designed by AW Harrison and produced by Fletcher's Ultralights of Turlock, California, in the late 1990s and early 2000s. The aircraft was supplied as a kit for amateur construction and was also available as a completed aircraft.
The V-STOL Pairadigm is an American twin-engine center-line thrust STOL homebuilt aircraft that was designed and produced by V-STOL Aircraft Corporation of Fort Myers, Florida, introduced in the late 1990s. When it was available the aircraft was supplied as a kit for amateur construction.