Douglas DC-9

First flight year — 1965

Douglas DC-9 Specifications


	DC-9-30	DC-9-50

Dimensions
Length (m)	36.4	40.7
Wingspan (m)	28.5	28.5
Height (m)	8.4	8.4
Wing area (m2)	93	93
Weight
Maximum take-off weight (kg)	49 900	54 400
Maximum landing weight (kg)	45 800	49 900
Operating empty weight (kg)	25 400	29 300
Maximum zero fuel weight (kg)	39 460	44 670
Maximum payload (kg)	16 300	15 400
Standard fuel capacity (litres)	13 900	16 100
Performance
Range with max payload (km)	2 200	1 850
Cruise speed (km/h)	910	900
Maximum operating altitude (m)	10 700	10 700
Take-off field length (m)	1 800	2 360
Landing field length (m)	1 300	1 440
Engines	P&W JT8D-7, 2 x 14000 lb	P&W JT8D-15, 2 x 15500 lb P&W JT8D-17, 2 x 16200 lb
Cabin Data
Passengers (1-class)	119	139
Passengers (2-class)	105	125
Cabin width (m)	3.14	3.14