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LUS-222

From Wikipedia, the free encyclopedia
LUS-222
Role Utility aircraft
National origin Portugal
Manufacturer EEA Aircraft and Maintenance, S.A. and CEiiA (Centro de Engenharia e Desenvolvimento de Produtos)
First flight 2027
Status Under development
Developed from Desaer ATL-100

The LUS-222 is a twin-turboprop, high-wing, utility aircraft under development by EEA Aircraft and Maintenance, S.A. in Portugal.[1]

Specifications

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General characteristics

  • Capacity: 19 passengers/5,000 lb (2,000kg) payload (commuter)
  • Length: 55 ft 1 in (16.80 m)
  • Wingspan: 72 ft 3 in (22.02 m)
  • Height: 20 ft 8 in (6.30 m)
  • Wing area: 441.0 sq ft (40.97 m2)
  • Aspect ratio: 11.8
  • Empty weight: 12,325 lb (5,591 kg) , Freighter: 11,000 lb (4,990 kg)
  • Max takeoff weight: 19,000 lb (8,618 kg)
  • Fuel capacity: 4,826 lb (2,000 kg) / ~720 gal (2,725 L)
  • Powerplant: 2 × Pratt & Whitney Canada PT6A-65SC turboprop, 1,110 hp (830 kW) each
  • Propellers: 4-bladed

Performance

  • Cruise speed: 210 kn (240 mph, 390 km/h) maximum
  • Range: 386 nmi (444 mi, 715 km) with 19 passengers, LRC, 100nmi IFR reserves, FL100
  • Ferry range: 1,100 nmi (1,200 mi, 2,000 km)
  • Service ceiling: 25,000 ft (7,600 m)
  • Takeoff Distance : 3,660 ft (1,116 m)[1]

References

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  1. ^ a b "ARL LUS 222". www.aeronextportugal.pt.