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Bombardier DHC-8 Dash-8

 

Developing Nation: Canada. Designer: de Havilland Canada, (Canadair) First Flight: - DHC-8-100: June 20, 1983 C-GDNK. - DHC-8-200: November 1994 C-GFBW. - DHC-8-300: May 1987 C-GDNK. - DHC-8-400: January 31, 1998 C-FJJA. First Delivery: October 23, 1984 to NorOntair, Canada.   DHC-8-100 / Q200 Crew: 2. Passengers: 37-39. Wing Span: 25,90 m. Wing Area: 54,40 m². Length: 22,30 m. Height: 7,49 m. Engine(s): - DHC 8-100: 2x Pratt & Whitney Canada PW121 turboprops. - DHC 8 Q200: 2x Pratt & Whitney Canada PW123C/D turboprops. Weight: - DHC 8-100: 10.250 kg. - DHC 8 Q200: 10.434 kg. Max. Take off weight: 16.465 kg. Max. Landing weight: - DHC 8-100: 15.377 kg. - DHC 8 Q200: 15.649 kg. Cruise Speed: - DHC 8-100: 440 Km/h. - DHC 8 Q200: 440 Km/h. Max. Speed: - DHC 8-100: 496 Km/h. - DHC 8 Q200: 546 Km/h. Operating altitude: 7.620 m. Max. Range: - DHC 8-100: 1.520 km. - DHC 8 Q200: 1.795 km.     DHC-8 Q300 Crew: 2. Passengers: 50. Wing Span: 27,43 m. Wing Area: 56,20 m². Length: 25,68 m. Height: 7,49 m. Engine(s): - Q300: 2x Pratt & Whitney Canada PW123A turboprops with 2380 Hp. - Q300B: or 2x Pratt & Whitney Canada PW123B turboprops with 2500 Hp. Weight: - Q300: 11.657 kg. - Q300B: 11.719 kg. Max. Take off weight: - Q300: 18.642 kg. - Q300B: 19.505 kg. Max. Landing weight: 19.051 kg. Max. Speed: - Q300: 532 Km/h. - Q300B: 528 Km/h. Operating altitude: 7.620 m. Max. Range: - Q300: 1.538 Km. - Q300B: 1.625 km.     DHC-8 Q400 Crew: 2. Passengers: 70. Wing Span: 28,42 m. Wing Area: 63,10 m². Length: 32,84 m. Height: 8,38 m. Engine(s): 2x Pratt & Whitney Canada PW150A turboprops with 4573 Hp. Weight: 16.580 kg. Max. Take off weight: 27.330 kg. Max. Landing weight: 26.600 kg. Max. Speed: 648 Km/h. Operating altitude: 7.620 m. Max. Range: 2.400 km.