DC-9-10

Aircraft type

Data given for the Douglas DC-9-10 in basic configuration.

Manufacturer Douglas
Aircraft family Airplane
Engine type Turbofan
Engine count 2
ICAO code DC91

Technical specifications

Dimensions
Fuselage height
3.61 m
11.84 ft
Fuselage width
3.35 m
10.99 ft
Height
8.4 m
27.56 ft
Length
31.82 m
104.4 ft
Wingspan
27.25 m
89.4 ft
Fuel
Fuel capacity
13,979 l
3,690 us gal
Speed limits
Mle
0.51
Mlo
0.51
Mmo
0.86
Vle
215 kt
398 km/h / 247 mph
Vlo
215 kt
398 km/h / 247 mph
Weight limits
MLW
37,059 kg
81,700 lb
MTOW
41,141 kg
90,700 lb
MTW
41,504 kg
91,500 lb
MZFW
33,566 kg
74,000 lb
OEW
22,300 kg
49,160 lb

Engine models

Manufacturer Name Cont. T/O
Pratt & Whitney JT8D-1 56.05 kN 62.28 kN
Pratt & Whitney JT8D-11 56.05 kN 66.72 kN
Pratt & Whitney JT8D-15 61.16 kN 68.95 kN
Pratt & Whitney JT8D-17 67.61 kN 71.17 kN
Pratt & Whitney JT8D-1A 56.05 kN 62.28 kN
Pratt & Whitney JT8D-1B 56.05 kN 62.28 kN
Pratt & Whitney JT8D-5 54.49 kN 54.49 kN
Pratt & Whitney JT8D-7 56.05 kN 62.28 kN
Pratt & Whitney JT8D-7A 56.05 kN 62.28 kN
Pratt & Whitney JT8D-7B 56.05 kN 62.28 kN
Pratt & Whitney JT8D-9 56.05 kN 64.50 kN
Pratt & Whitney JT8D-9A 56.05 kN 64.50 kN