Marawing 1-L Malamut

{{Short description|Czech ultralight aircraft}}

{{Use dmy dates|date=December 2022}}

{{Use British English|date=December 2022}}

{{Infobox Aircraft Begin

| name=1-L Malamut

| image=

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}}{{Infobox Aircraft Type

| type=Ultralight aircraft

| national origin=Czech Republic

| manufacturer=Marawing

| designer=

| first flight=

| introduced=

| retired=

| status=In production (2012)

| primary user=

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| developed from= Piper J-3 Cub

| variants with their own articles=

}}

The Marawing 1-L Malamut is a Czech ultralight aircraft, designed and produced by Marawing of Kolín. The aircraft is supplied as a complete ready-to-fly-aircraft.Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 65. WDLA UK, Lancaster UK, 2011. ISSN 1368-485XTacke, Willi; Marino Boric; et al: World Directory of Light Aviation 2015-16, page 66. Flying Pages Europe SARL, 2015. {{ISSN|1368-485X}}

Design and development

The Malamut was developed from the classic Piper J-3 Cub. It was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a strut-braced high-wing, a two-seats-in-tandem enclosed cockpit, fixed conventional landing gear and a single engine in tractor configuration.

The aircraft is constructed in the same manner as the Cub. The fuselage is made from welded steel tubing, while the wings have a wooden structure, all covered in doped aircraft fabric. Its {{convert|10.1|m|ft|1|abbr=on}} span wing has an area of {{convert|15.1|m2|sqft|abbr=on}} and flaps. The standard engine available is the {{convert|80|hp|kW|0|abbr=on}} Rotax 912UL four-stroke powerplant.

Specifications (1-L Malamut)

{{Aircraft specs

|ref=Bayerl & Tacke

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|crew=one

|capacity=one passenger

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|empty weight kg=295

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|gross weight kg=472.5

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|fuel capacity={{convert|160|L}}

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|eng1 number=1

|eng1 name=Rotax 912UL

|eng1 type=four cylinder, liquid and air-cooled, four stroke aircraft engine

|eng1 kw=60

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|max speed kmh=198

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|cruise speed kmh=165

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|stall speed kmh=50

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|wing loading kg/m2=31.3

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References

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