De Havilland Canada DHC-5 Buffalo

· Boeing

Airplanes

Length

24.0792 m

Flat Wing Span

29.2608 m

Height

8.5344 m

Flat Wing Area

87.7934 m²

Flat Wing Aspect Ratio

9.75

Max Seating

Cruise Speed

420.4036 km/h

Max Ceiling

9448.8 m

Number of Engines

First Flight

1964-04-09

Entry Into service

1965-01-01

Number Built

122

Maximum Take-Off Weight

22.3167 t (paragliders: kg)

Total Fuel Capacity

7978.388

Maximum Range

1111.2 km

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
De Havilland Canada DHC-5 Buffalo	22.3167	7978.388	1111.2

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Antonov An-30		24.26	29.2		Compare
Xi'an Y-7		24.218	29.666	52	Compare
Xi'an MA60		24.71	29.2	62	Compare
Xi'an MA600		24.71	29.2	60	Compare
Hawker Siddeley Andover		23.7744	29.8704	52	Compare
Antonov An-24	Ivchenko AI-24	23.53	29.2	50	Compare

All data (28 fields)

Name: De Havilland Canada DHC-5 Buffalo
Manufacturer: Boeing
Description: The de Havilland Canada DHC-5 Buffalo is a short takeoff and landing (STOL) utility transport turboprop aircraft developed from the earlier piston-powered DHC-4 Caribou.
ICAO Code: DHC5
First Flight: 1964-04-09
Entry Into service: 1965-01-01
Production End: 1972-01-01
Designer: Boeing
Type: Utility aircraft
Length (m): 24.0792
Height (m): 8.5344
Cockpit Crew: 3
Max Seating: 41
Cruise Speed (km/h): 420.4036
Min Speed (km/h): 135.1959
Max Ceiling (m): 9448.8
Rate of Climb (m/s): 9.2456
Capacity Description: 41 troops or 24 stretchers or 18000 lb payload
Number Built: 122
Powerplant Description: 2 × General Electric CT64-820-4 turboprop engines, 2336 kW (3133 hp) each
Primary Users: Royal Canadian Air Force (historical)
Status: In limited service
Wikipedia Article (URL): en.wikipedia.org/wiki/De_Havilland_Canada_DHC-5_Buffalo
Flat Wing Span (m): 29.2608
Flat Wing Area (m²): 87.7934
Flat Wing Aspect Ratio: 9.75
Wake Category: M
Number of Engines: 2