Comparison of Short C-23 Sherpa and Sukhoi Su-80

Attribute	Sukhoi Su-80 ×	Short C-23 Sherpa ×
General
Manufacturer	Sukhoi	Short Brothers
Model	Sukhoi Su-80	Short C-23 Sherpa
Country	Russia	United Kingdom
Manufactured from (year)	2006	1984
Manufactured to (year)	-	1990
Type	Passenger Turbo Props	Military Propellor Planes
Icao	SU80	SH33
Performance
Engine	2x 2 X General Electric GE CT7-9B Turboprop	2x Pratt & Whitney Canada PT6A
Power, hp (hp)	1,750	1,198
Avionics	SBKV-P strapdown heading and altitude system, VIM-95C (VOR/ILS/SP/MRK) navigation and landing systems	-
Max cruise speed (km/h)	463	409
Approach speed (km/h)	-	141
Travel range (km)	1,408	1,241
Fuel economy (km/l)	0.597	-
Service ceiling (m)	7,590	8,230
Rate of climb (m/sec)	-	5.99
Take off distance (m)	840	1,036
Landing distance (m)	460	1,225
Weights
Max take off weight (kg)	13,500	11,612
Max landing weight (kg)	13,550	11,385
Max payload (kg)	2,730	3,302
Fuel tank capacity (l)	2,498	2,035
Baggage volume (m³)	-	34.8
Dimensions
Seats	3	3
Cabin height (m)	1.82	1.95
Cabin width (m)	2.17	1.95
Cabin length (m)	7.75	9.09
Exterior length (m)	18.26	17.69
Tail height (m)	5.74	4.95
Fuselage diameter (m)	2.4	2.2
Wing span (m)	23.18	22.78
Wing tips	Blended Tips	No Winglets