Samiksha Jaiswal (Editor)

Flight Design MC

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Top speed
  
220 km/h

Wingspan
  
9.5 m

Weight
  
360 kg

Engine type
  
Rotax 912

Range
  
950 km

Cruise speed
  
210 km/h

Unit cost
  
99,998–99,998 USD (2011)

Flight Design MC httpsuploadwikimediaorgwikipediacommonsthu

Prototype testing of the flight design mc


The Flight Design MC (Metal Concept) is a German light-sport aircraft, designed and produced by Flight Design, introduced at AirVenture in 2008. The aircraft is supplied as a complete ready-to-fly-aircraft.

Contents

Checking out in the flight design mc light sport airplane


Design and development

The MC design was based on the general shape of the CT series, but rendered in metal and with a strut-braced wing, in place of the CT series' composite construction and cantilever wing. The design goal was to provide a more robust design, primarily for flight school use. The resulting MC has a lower cruise speed as well as less payload and range than the comparable Flight Design CTLW.

The MC was designed to comply with US light-sport aircraft rules. It features a strut-braced high-wing, a two-seats-in-side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.

The MC's structure is totally different from the CT series. Aircraft fuselage is made from welded steel tubing forming a safety cage around the cockpit, with crumple zones built in. The wings and tail are predominantly aluminum sheet. Its 9.5 m (31.2 ft) has an area of 11.3 m2 (122 sq ft) and flaps. The landing gear legs are composite and are adapted from the CTLS. To simplify fuel management the wing fuel tanks all feed via a single lever fuel supply system. A ballistic parachute is standard equipment. Standard engines available are the 80 hp (60 kW) Rotax 912UL and the 100 hp (75 kW) Rotax 912ULS and Rotax 912iS four-stroke powerplants.

Variants

MCi
Version with the Rotax 912iS 100 hp (75 kW) engine.

Specifications (MC)

Data from Bayerl

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Wingspan: 9.5 m (31 ft 2 in)
  • Wing area: 11.3 m2 (122 sq ft)
  • Empty weight: 360 kg (794 lb)
  • Gross weight: 600 kg (1,323 lb)
  • Fuel capacity: 100 litres (22 imp gal; 26 US gal)
  • Powerplant: 1 × Rotax 912UL four cylinder, liquid and air-cooled, four stroke aircraft engine, 60 kW (80 hp)
  • Performance

  • Maximum speed: 220 km/h (137 mph; 119 kn)
  • Cruise speed: 210 km/h (130 mph; 113 kn)
  • Stall speed: 65 km/h (40 mph; 35 kn)
  • Rate of climb: 5 m/s (980 ft/min)
  • References

    Flight Design MC Wikipedia