IAC MA-2 MAMBA

 

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