BRAND and MODEL
IAC MA-2 MAMBA
TYPE
Two-seat utility aircraft
ORIGIN
Australia
ENGINE
(MA-2A)
One 119 kw (160 hp) Textron Lycoming O-320-D1A four-cylinder horizontally-opposed air-cooled engine
SPECIFICATIONS
Wingspan: 8.36 m (27 ft 5 in)
Length: 7.47 m (24 ft 6 in)
Height: 2.74 m (9 ft)
Wing area: 9.29 m² (100 sq ft)
Max speed at sea level: 232 k/h (144 mph)
Max cruising speed at 70% power: 213 km/h (132 mph)
Max cruising speed at 2,440 m (8,000 ft): 222 km/h (138 mph)
Max rate of climb at sea level: 335 m/min (1,100 ft/min)
Stalling speed flaps down: 84 km/h (52 mph)
Range at 2,440 m (8,000 ft) at max cruising speed, no reserve: 1,262 km (787 miles)
Empty weight: 635 kg (1,400 lb)
Loaded weight: 967 kg (2,000 lb)
PHOTO
Source of phothograph
