McDonnell Douglas DC-9

The McDonnell Douglas DC-9 is a twin-engine, short-range jet airliner seating 110 passengers.
Specifications
+ DC-9 airplane characteristics Variant -15 (-21)  -32  -41  -51 Cockpit crew Two 1-class seating 90Y@31-32" 115Y@31-33" 125@31-34" 135@32-33" Exit limit 109 127 128  139 Cargo 600 ft³ / 17.0m³-15F: 2,762 ft³ / 78.2m³ 895 ft³ / 25.3m³-33F: 4,195 ft³ / 119.0m³ 1,019 ft³ / 28.9m³ 1,174 ft³ / 33.2m³ Length 104 ft 4.8in / 31.82m 119 ft 3.6in / 36.36m 125 ft 7.2in / 38.28m 133 ft 7in / 40.72m Wingspan 89 ft 4.8in / 27.25m-21:  93 ft 3.6in / 28.44m 93 ft 3.6in / 28.44m 93 ft 4.2in / 28.45m Height 27 ft 7in / 8.4m 27 ft 9in / 8.5m 28 ft 5in / 8.7m 28 ft 9in / 8.8m Fuselage width 131.6in / 334.3 cm Cabin width in / cm Max. takeoff 90,700 lb / 41,141 kg-21: 98,000 lb / 45,359 kg 108,000 lb / 48,988 kg 114,000 lb / 51,710 kg 121,000 lb / 54,885 kg Max. Landing -21:     Empty 49,162 lb / 22,300 kg-15F: 53,200 lb / 24,131 kg-21: 52,644 lb / 23,879 kg 56,855 lb / 25,789 kg-33F: 56,430 lb / 25,596 kg 61,335 lb / 27,821 kg 64,675 lb / 29,336 kg  Fuel 24,743 lb / 11,223 kg 24,649 lb / 11,181 kg Engine (2×) JT8D-1(A/B) -5 -7(B) -9(A) -11 -15 -17; -21: -9(A) -11 -1(A/B) -5 -7(A/B) -9(A) -11 -15(A) -17(A) -9(A) -11 -15(A) -17(A) -15(A) -17(A) Thrust (2×) -1(A/B) -7(A/B) : , -5/-9(A): , -11: , -15(A): , -17(A) :  Ceiling  MMo  Range -21:    

References

Category:Douglas aircraft