Comparison of de Havilland DHC-8-200 and Sukhoi Su-80

Attribute	de Havilland DHC-8-200 ×	Sukhoi Su-80 ×
General
Manufacturer	de Havilland	Sukhoi
Model	de Havilland DHC-8-200	Sukhoi Su-80
Country	United Kingdom	Russia
Manufactured from (year)	1983	2006
Type	Passenger Turbo Props	Passenger Turbo Props
Icao	DH8B	SU80
Performance
Engine	2x Pratt & Whitney Canada PW123	2x 2 X General Electric GE CT7-9B Turboprop
Power, hp (hp)	2,150	1,750
Avionics	Honeywell SPZ-8000 dual-channel digital AFCS, Primus P660 weather radar, Collins nav/comm systems	SBKV-P strapdown heading and altitude system, VIM-95C (VOR/ILS/SP/MRK) navigation and landing systems
Max cruise speed (km/h)	537	463
Travel range (km)	2,084	1,408
Fuel economy (km/l)	-	0.597
Service ceiling (m)	7,620	7,590
Rate of climb (m/sec)	7.49	-
Take off distance (m)	1,000	840
Landing distance (m)	780	460
Weights
Max take off weight (kg)	16,466	13,500
Max landing weight (kg)	15,649	13,550
Max payload (kg)	4,647	2,730
Fuel tank capacity (l)	3,161	2,498
Baggage volume (m³)	8.5	-
Dimensions
Seats	4	3
Cabin height (m)	1.95	1.82
Cabin width (m)	2.5	2.17
Cabin length (m)	9.16	7.75
Exterior length (m)	22.25	18.26
Tail height (m)	7.5	5.74
Fuselage diameter (m)	2.69	2.4
Wing span (m)	25.9	23.18
Wing tips	No Winglets	Blended Tips