Comparison of McDonnell Douglas DC-9-10 and Fokker 100

Attribute	Fokker 100 ×	McDonnell Douglas DC-9-10 ×
General
Manufacturer	Fokker	Douglas Aircraft Co.
Model	Fokker 100	McDonnell Douglas DC-9-10
Country	Netherlands	United States
Manufactured from (year)	1986	1965
Manufactured to (year)	1997	1969
Type	Mid Size Passenger Jets	Light Passenger Jets
Icao	F100	DC91
Performance
Engine	2x 2 × Rolls-Royce Tay Mk.650 Turbofans	2x Pratt & Whitney JT8D-7
Power, lbf (lbf)	15,100	14,000
Avionics	Rockwell Collins DU-1000 EFIS	-
Max cruise speed (km/h)	845	896
Approach speed (km/h)	222	244
Travel range (km)	3,111	2,685
Fuel economy (km/l)	0.235	-
Service ceiling (m)	10,668	10,668
Rate of climb (m/sec)	15.24	14.22
Take off distance (m)	1,855	1,615
Landing distance (m)	1,320	1,320
Weights
Max take off weight (kg)	45,810	41,100
Max landing weight (kg)	39,915	37,100
Max payload (kg)	11,993	18,000
Fuel tank capacity (l)	13,366	13,979
Baggage volume (m³)	24	17
Dimensions
Seats	122	9
Seats - business class	17	-
Seats - first class	85	-
Cabin height (m)	2.01	2.1
Cabin width (m)	3.1	3.1
Cabin length (m)	20.8	18.29
Exterior length (m)	35.53	31.82
Tail height (m)	8.5	8.38
Fuselage diameter (m)	3.3	3.34
Wing span (m)	28.08	27.25
Wing tips	No Winglets	No Winglets