Akoya Lisa Airplanes

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The LISA Akoya is a French single engine light aircraft, seating two in side-by-side configuration. It is an amphibious aircraft capable of alighting on land, water or snow without adaptation. It has a high aspect ratio folding wing, with trailing edge extensions rather than flaps, and a rear mounted tractor configuration engine. General characteristics Capacity: 2 Length: 6.90 m (22 ft 8 in) Wingspan: 11.00 m (36 ft 1 in) Height: 2.35 m (7 ft 9 in) including propeller Wing area: 6.70 m2 (72.1 sq ft) Empty weight: 400 kg (882 lb) Max takeoff weight: 650 kg (1,433 lb) Fuel capacity: 70 LO (18.5 USgal, 15.4 Impgal) with optional additional 110 L (29 US gal, 24.2 Imp gal) tank [13] Powerplant: 1 × Rotax 912 ULS flat four cylinder piston with 1:2.34 reduction gear, 73.5 kW (98.6 hp) Propellers: 3-bladed Performance Cruising speed: 210 km/h (130 mph; 113 kn) economical Stall speed: 64 km/h (40 mph; 35 kn) flaps down Never exceed speed: 290 km/h (180 mph; 157 kn) Range: 1,250[13] km (777 mi; 675 nmi) at economical cruising speed without optional tank Rate of climb: 5.2 m/s (1,020 ft/min) maximum Avionics VHF, intercom, transponder. Two screen EFIS with emergency backup instruments.