Marawing 1-L Malamut
# Marawing 1-L Malamut

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.

## 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 10.1 m (33.1 ft) span wing has an area of 15.1 $m^2$ (163 sq ft) and flaps. The standard engine available is the 80 hp (60 kW) Rotax 912UL four-stroke powerplant.

## Specifications (1-L Malamut)

Data from Bayerl & Tacke

General characteristics

* Crew: one
* Capacity: one passenger
* Wingspan: 10.1 m (33 ft 2 in)
* Wing area: 15.1 $m^2$ (163 sq ft)
* Empty weight: 295 kg (650 lb)
* Gross weight: 472.5 kg (1,042 lb)
* Fuel capacity: 160 litres (35 imp gal; 42 US gal)
* Powerplant: 1 × Rotax 912UL four cylinder, liquid and air-cooled, four stroke aircraft engine, 60 kW (80 hp)

Performance

* Maximum speed: 198 km/h (123 mph, 107 kn)
* Cruise speed: 165 km/h (103 mph, 89 kn)
* Stall speed: 50 km/h (31 mph, 27 kn)
* Rate of climb: 5 m/s (980 ft/min)
* Wing loading: 31.3 $kg/m^2$ (6.4 lb/sq ft)
