BRAND and MODEL
TRANSAVIA PL-12 MIL
TYPE
Multi-role utility aircraft
ORIGIN
Australia
ENGINE
One Textron Lycoming 298 kw (400 hp) IO-720-D1BD eight-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan [upper]: 11.98 m (39 ft 3½ in)
Stub wing span: 4.93 m (16 ft 2 in)
Length: 7.37 m (24 ft 2 in)
Height: 2.87 m (9 ft 5 in)
Wing area: 26.76 m² (288 sq ft)
Max speed at 915 m (3,000 ft): 202 km/h (125 mph)
Max cruising speed at 75% power: 191 km/h (118 mph)
Stalling speed power off flaps up: 97 km/h (60 mph)
Stalling speed flaps down: 73 km/h (45 mph)
Max rate of climb at sea level: 168 m/min (550 ft/min)
Max light-weight rate of climb: 488 m/min (1,600 ft/min)
Service ceiling: 6,890 m (22,600 ft)
Take-off run: 275 m (900 ft)
Landing run: 78 m (255 ft)
Fuel capacity: 189 litres (41.5 imp gals)
Fuel capacity with optional long-range tank: 364 litres (80.1 imp gals)
Empty weight: 1,111 kg (2,450 lb)
Max take-off weight in agricultural category: 2,227 kg (4,910 lb)
PHOTO
eBay:Source of phothograph
