BRAND and MODEL
GROB G-115
TYPE
Two-seat training and touring aircraft
ORIGIN
Germany
ENGINE
One 119 kw (160 hp) Textron Lycoming O-320-D1A four-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan: 10 m (32 ft 9½ in)
Length: 7.44 m (24 ft 5 in)
Height: 2.75 m (9 ft 0¼ in)
Wing area: 12.21 m² (131.4 sq ft)
Max speed at sea level: 317 km/h (196 mph)
Cruising speed at 75% power: 240 km/h (149 mph)
Max rate of climb at sea level: 387 m/min (1,270 ft/min)
Stalling speed flaps down: 85 km/h (53 mph)
Service ceiling: 4,875 m (16,000 ft)
Range with max fuel, no reserve: 1,204 km (748 miles)
Empty weight: 650 kg (1,433 lb)
Loaded weight: 920 kg (2,028 lb)
PHOTO
flugzeuginfo.net:Source of phothograph
