Light Wing AC4

Source: Wikipedia, the free encyclopedia.

AC4
Role
Ultralight aircraft and Light-sport aircraft
National origin Switzerland
Manufacturer Light Wing AG
Designer Hans Gygax
Introduction 2013
Status In production (2019)

The Light Wing AC4 is a

ultralight and light-sport aircraft, designed by Hans Gygax and produced by Light Wing AG of Stans. The aircraft was publicly introduced at the AERO Friedrichshafen show in 2013. It is supplied complete and ready-to-fly.[1][2][3]

Design and development

The AC4 was designed to comply with the

side-by-side configuration enclosed cockpit, fixed tricycle landing gear and a single engine in tractor configuration.[1][2]

The aircraft is made from a combination of composites and

The AC4 can accommodate one pilot and one passenger and was also designed for

European Aviation Safety Agency type certification to the Certification Specification for Light Sport Aeroplanes (CS-LSA) on 6 August 2015.[5][1][2]

Specifications (AC4 LSA)

Data from Bayerl, Tacke and manufacturer[1][2][4]

General characteristics

  • Crew: one
  • Capacity: one passenger
  • Length: 7.04 m (23 ft 1 in)
  • Wingspan: 9.60 m (31 ft 6 in)
  • Height: 2.67 m (8 ft 9 in)
  • Wing area: 16.65 m2 (179.2 sq ft)
  • Empty weight: 350 kg (772 lb)
  • Gross weight: 600 kg (1,323 lb)
  • Fuel capacity: 100 litres (22 imp gal; 26 US gal)
  • Powerplant: 1 ×
    four stroke aircraft engine
    , 75 kW (101 hp)
  • Propellers: 3-bladed composite

Performance

References

  1. ^ a b c d e Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 63. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
  2. ^
    ISSN 1368-485X
  3. ^ Light Wing AG. "Company". lightwing.ch. Retrieved 27 August 2016.
  4. ^ a b Light Wing AG. "Lightwing AC4". lightwing.ch. Retrieved 27 August 2016.
  5. ^ TYPE-CERTIFICATE DATA SHEET EASA.A.588 for LIGHTWING AC4 (PDF). EASA. 6 August 2015. Retrieved 12 February 2019.