Comparison of Fokker 50 and Short 360

Attribute	Fokker 50 ×	Short 360 ×
General
Manufacturer	Fokker	Short Brothers
Model	Fokker 50	Short 360
Country	Netherlands	United Kingdom
Manufactured from (year)	1987	1980
Manufactured to (year)	1997	1991
Type	Passenger Turbo Props	Passenger Turbo Props
Icao	F50	SH36
Performance
Engine	2x Pratt & Whitney PW125B turboprops	2x Pratt & Whitney Canada PT6A-65AR
Power, hp (hp)	2,500	1,424
Avionics	EFIS and Automatic Flight Control System	-
Max cruise speed (km/h)	530	404
Approach speed (km/h)	180	185
Travel range (km)	2,056	1,056
Fuel economy (km/l)	0.44	-
Service ceiling (m)	7,620	6,096
Rate of climb (m/sec)	7.62	4.84
Take off distance (m)	1,350	1,300
Landing distance (m)	1,130	1,100
Weights
Max take off weight (kg)	20,820	12,300
Max landing weight (kg)	20,030	12,020
Max payload (kg)	5,500	3,500
Fuel tank capacity (l)	5,137	2,180
Baggage volume (m³)	16.72	-
Dimensions
Seats	62	39
Cabin height (m)	1.96	1.88
Cabin width (m)	2.5	1.85
Cabin length (m)	15.63	8.4
Exterior length (m)	25.25	21.6
Tail height (m)	8.32	7.27
Fuselage diameter (m)	2.7	2.2
Wing span (m)	29	22.8
Wing tips	No Winglets	No Winglets