Comparison of Fokker 100 and McDonnell Douglas DC-9-20

Attribute	Fokker 100 ×	McDonnell Douglas DC-9-20 ×
General
Manufacturer	Fokker	McDonnell Douglas
Model	Fokker 100	McDonnell Douglas DC-9-20
Country	Netherlands	United States
Manufactured from (year)	1986	1965
Manufactured to (year)	1997	1982
Type	Mid Size Passenger Jets	Mid Size Passenger Jets
Icao	F100	DC92
Performance
Engine	2x 2 × Rolls-Royce Tay Mk.650 Turbofans	2x JT8D-11
Power, lbf (lbf)	15,100	15,000
Avionics	Rockwell Collins DU-1000 EFIS	-
Max cruise speed (km/h)	845	898
Approach speed (km/h)	222	235
Travel range (km)	3,111	2,778
Fuel economy (km/l)	0.235	-
Service ceiling (m)	10,668	10,668
Rate of climb (m/sec)	15.24	12.7
Take off distance (m)	1,855	1,600
Landing distance (m)	1,320	1,500
Weights
Max take off weight (kg)	45,810	45,359
Max landing weight (kg)	39,915	43,227
Max payload (kg)	11,993	11,501
Fuel tank capacity (l)	13,366	13,926
Baggage volume (m³)	24	17
Dimensions
Seats	122	9
Seats - business class	17	-
Seats - first class	85	-
Cabin height (m)	2.01	2.05
Cabin width (m)	3.1	3.12
Cabin length (m)	20.8	18.29
Exterior length (m)	35.53	31.82
Tail height (m)	8.5	8.4
Fuselage diameter (m)	3.3	3.35
Wing span (m)	28.08	28.44
Wing tips	No Winglets	No Winglets