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De Havilland Canada DHC-5 Buffalo ✕ Xi'an MA600 ✕
Manufacturer Boeing Xi'an Aircraft Industrial Corporation
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. The Xi'an MA600 (MA for "Modern Ark", ) is an improved version of the Xi'an MA60 manufactured by the Xi'an Aircraft Industrial Corporation under the Aviation Industry Corporation of China (AVIC).
ICAO Code DHC5
First Flight 1964-04-09 2008-10-10
Entry Into service 1965-01-01 2010-01-01
Production End 1972-01-01
Designer Boeing Avic
Type Utility aircraft
Length (m) 24.0792 24.71
Height (m) 8.5344 8.858
Cockpit Crew 3 2
Max Seating 41 60
Max Speed (km/h) 514
Cruise Speed (km/h) 420.4036 430
Min Speed (km/h) 135.1959
Max Ceiling (m) 9448.8 7622
Rate of Climb (m/s) 9.2456
Capacity Description 41 troops or 24 stretchers or 18000 lb payload 60 passengers
National Origin China
Number Built 122 18
Powerplant Description 2 × General Electric CT64-820-4 turboprop engines, 2336 kW (3133 hp) each 2 × Pratt & Whitney Canada PW127J turboprop engines, 2148 kW (2881 hp) each
Primary Users Royal Canadian Air Force (historical) Civil Aviation Administration of China, Laos Government , Malawi Air Force , Lao Skyway
Status In limited service In service
Wikipedia Article (URL) en.wikipedia.org/wiki/De_Havilland_Canada_DHC-5_Buffalo en.wikipedia.org/wiki/Xi%27an_MA600
Flat Wing Span (m) 29.2608 29.2
Flat Wing Area (m²) 87.7934
Flat Wing Aspect Ratio 9.75
Wake Category M
Number of Engines 2 2