The Buladocga was first developed in 1973 by the Leofred Aircraft Co. to provide the Nova English Airforce with a basic trainer. However during this early period a number of these planes were converted by the NERAF to provide basic ground support for infantry units fighting in the mountainous regions of East Moorland. Since then the planes continued their multi-role status until the collapse of the Faedertellus.
Specifications;
General characteristics
Crew: 2: student, instructor Length: 23 ft 3 in (7.08 m) Wingspan: 33 ft 0 in (10.06 m) Height: 7 ft 5¾ in (2.28 m) Wing area: 129.4 ft² (12.02 m²) Aspect ratio: 8.4:1 Empty weight: 1,475 lb (669 kg) Useful load: 920 lb (417 kg) Max. takeoff weight: 2,350 lb (1,066 kg)
Performance
Never exceed speed: 210 knots (241 mph, 389 km/h) Maximum speed: 130 knots (150 mph, 241 km/h) at sea level Stall speed: 54 knots (62 mph, 100 km/h) Range: 540 nmi (621 mi, 1,000 km) Service ceiling: 16,000 ft (4,875 m) Rate of climb: 1,034 ft/min (5.25 m/s)
Armament
Hardpoints: 4 underwing hardpoints with a capacity of; Inner hardpoints: 150 kg (330 lb) each Outer hardpoints:100 kg (220 lb) each Maximum external load: 300 kg (660 lb)