McDonnell Douglas DC-9
Specifications

McDonnell Douglas DC-9

Section Title: Specifications
Table Section Text: None

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	122.4in / 311cm

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	81,700 lb (37,058 kg) 21: 95,300 lb (43,227 kg)	99,000 lb (44,906 kg)	102,000 lb (46,266 kg)	110,000 lb (49,895 kg)

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) : 14,000 lbf (62 kN), -5/-9(A): 12,250 lbf (54.5 kN), -11: 15,000 lbf (67 kN), -15(A): 15,500 lbf (69 kN), -17(A) : 16,000 lbf (71 kN)

Ceiling	35,000 ft (11,000 m)

MMo	Mach 0.84 (484 kn; 897 km/h)

Range	1,300 nmi (2,400 km) 21: 1,500 nmi (2,800 km)	1,500 nmi (2,800 km)	1,200 nmi (2,200 km)	1,300 nmi (2,400 km)

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