Crew: two
Capacity: two seats side by side under rearward-sliding canopy with provision for a third seat in rear of cabin
Length: 29 ft 01⁄2 in (8.55 m)
Wingspan: 38 ft 71⁄2 in (11.77 m)
Height: 9 ft 1 in (2.77 m)
Wing area: 249 sq ft (23.1 m2)
Airfoil: NACA 23015 at root, NACA 23010 at tip
Aspect ratio: 6.0:1
Empty weight: 3,289 lb (1,495 kg)
Loaded weight: 4,265 lb (1,939 kg)
Powerplant: 1 x Alvis Leonides IV 126 9-cylinder radial engine, 550 hp (390 kW)
Maximum speed: 201 mph (174 knots, 323 km/h)
Cruise speed: 170 mph (147 knots, 273 km/h)
Stall speed: 53 mph (46 knots, 85 km/hr) (flaps down)
Endurance: 3.5 hours at 158 mph (137 knots; 254 km/h)
Service ceiling: 18,500 ft (5,640 m)
Rate of climb: 1,520 ft/min (7.7 m/s)
Take-off run to 50 ft (15 m): 1,000 ft (305 m) (standard temperature)
Landing run from 50 ft (15 m): 1,000 ft (305 m)
Basic trainer. Two prototypes, first flown 11 February 1949. 262 production aircraft built for RAAF during 1950-52.