BRAND and MODEL
GENERAL AIRCRAFT CORPORATION GAC-100
TYPE
Commercial airliner
ORIGIN
United States of America
ENGINE
Four 597 kw (800 shp) Pratt & Whitney PT6A-30 turboprops
SPECIFICATIONS
Wingspan: 21.34 m (70 ft)
Length: 19.61 m (64 ft 4 in)
Height: 6.71 m (22 ft)
Wing area: 64 m² (688.89 sq ft)
Max permissible diving speed: 613 km/h (380 mph)
Max cruising speed at sea level: 527 km/h (327 mph)
Economical cruising speed at 7,600 m (25,000 ft): 527 km/h (327 mph)
Stalling speed flaps up: 202 km/h (126 mph)
Stalling speed flaps down: 160 km/h (100 mph)
Rate of climb at sea level: 1,100 m/min (3,600 ft/min)
Service ceiling: 7,600 m (25,000 ft)
Service ceiling, one engine out: 5,200 m (17,050 ft)
Take-off run: 557 m (1,825 ft)
Take-off distance to 10.5 m (35 ft): 850 m (2,790 ft)
Landing distance from 10.5 m (25 ft): 698 m (2,290 ft)
Landing run: 442 m (1,450 ft)
Range with max fuel with 278 km (173 miles) diversion: 2,035 km (1,265 miles)
Range with 40 passengers, reserve as above: 648 km (403 miles)
Empty weight: 11,000 kg (24,250 lb)
Max payload weight: 2,830 kg (6,240 lb)
Loaded weight: 17,010 kg (37,501 lb)
PHOTO
secretprojects.co.uk:Source of phothograph
