DC-9-50

Aircraft type

Data given for the Douglas DC-9-51 in basic configuration.

Manufacturer Douglas
Aircraft family Airplane
Engine type Turbofan
Engine count 2
ICAO code DC95

Technical specifications

Dimensions
Fuselage height
3.61 m
11.84 ft
Fuselage width
3.35 m
10.99 ft
Height
8.6 m
28.22 ft
Length
40.72 m
133.6 ft
Wingspan
28.45 m
93.34 ft
Fuel
Fuel capacity
13,926 l
3,680 us gal
Speed limits
Mle
0.7
Mlo
0.7
Mmo
0.84
Vle
300 kt
556 km/h / 345 mph
Vlo
250 kt
463 km/h / 288 mph
Vmo
340 kt
630 km/h / 391 mph
Weight limits
MLW
49,895 kg
110,000 lb
MTOW
54,885 kg
121,000 lb
MTW
55,338 kg
122,000 lb
MZFW
44,679 kg
98,500 lb
OEW
29,336 kg
64,670 lb

Aircraft models

Manufacturer Name
Douglas DC-9-51

Engine models

Manufacturer Name Cont. T/O
Pratt & Whitney JT8D-15 61.16 kN 68.95 kN
Pratt & Whitney JT8D-15A 61.16 kN 68.95 kN
Pratt & Whitney JT8D-17 67.61 kN 71.17 kN
Pratt & Whitney JT8D-17A 67.61 kN 71.17 kN