Comparison of Fokker 100 and McDonnell Douglas DC-9-30

Attribute	McDonnell Douglas DC-9-30 ×	Fokker 100 ×
General
Manufacturer	McDonnell Douglas	Fokker
Model	McDonnell Douglas DC-9-30	Fokker 100
Country	United States	Netherlands
Manufactured from (year)	1965	1986
Manufactured to (year)	1982	1997
Type	Mid Size Passenger Jets	Mid Size Passenger Jets
Icao	DC93	F100
Performance
Engine	2x JT8D-11	2x 2 × Rolls-Royce Tay Mk.650 Turbofans
Power, lbf (lbf)	15,000	15,100
Avionics	-	Rockwell Collins DU-1000 EFIS
Max cruise speed (km/h)	898	845
Approach speed (km/h)	235	222
Travel range (km)	2,778	3,111
Fuel economy (km/l)	-	0.235
Service ceiling (m)	10,668	10,668
Rate of climb (m/sec)	10.16	15.24
Take off distance (m)	2,100	1,855
Landing distance (m)	1,500	1,320
Weights
Max take off weight (kg)	48,988	45,810
Max landing weight (kg)	44,906	39,915
Max payload (kg)	13,674	11,993
Fuel tank capacity (l)	13,926	13,366
Baggage volume (m³)	25.3	24
Dimensions
Seats	115	122
Seats - business class	-	17
Seats - first class	-	85
Cabin height (m)	2.05	2.01
Cabin width (m)	3.12	3.1
Cabin length (m)	22.79	20.8
Exterior length (m)	36.36	35.53
Tail height (m)	8.5	8.5
Fuselage diameter (m)	3.35	3.3
Wing span (m)	28.44	28.08
Wing tips	No Winglets	No Winglets