McDonnell Douglas DC-9

DC-9
	A Northwest Airlines DC-9-41, 2006
Role	Narrow-body jet airliner
Manufacturer	Douglas Aircraft Company ; McDonnell Douglas
First flight	February 25, 1965
Introduction	December 8, 1965 with Delta Air Lines
Status	In limited service
Primary users	USA Jet Airlines; Aeronaves TSM ; Northwest Airlines (historical) ; Delta Air Lines (historical)
Produced	1965–1982
Number built	976
Unit cost	US$5.2M (-40, 1972)[1]
Variants	McDonnell Douglas C-9
Developed into	McDonnell Douglas MD-80 ; McDonnell Douglas MD-90 ; Boeing 717

The McDonnell Douglas DC-9 is a twin-engine, short-range jet airliner seating 110 passengers.

Scandinavian Airlines McDonnell Douglas DC-9

Specifications

DC-9 airplane characteristics[2]
Variant	-15 (-21)	-32	-41	-51
Cockpit crew[3]^: 66	Two
1-class seating^: 15–18	90Y@31-32"	115Y@31-33"	125@31-34"	135@32-33"
Exit limit[3]^: 80	109	127	128	139
Cargo^: 4	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^: 5–9	104 ft 4.8in / 31.82m	119 ft 3.6in / 36.36m	125 ft 7.2in / 38.28m	133 ft 7in / 40.72m
Wingspan^: 10–14	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^: 10–14	27 ft 7in / 8.4m	27 ft 9in / 8.5m	28 ft 5in / 8.7m	28 ft 9in / 8.8m
Fuselage width^: 23	131.6in / 334.3 cm
Cabin width^: 24	122.4in / 311cm
Max. takeoff^: 4	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^: 4	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^: 4	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^: 4	24,743 lb / 11,223 kg	24,649 lb / 11,181 kg
Engine (2×)[3]	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×)[3]	-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[3]^: 67	35,000 ft (11,000 m)
MMo[3]	Mach 0.84 (484 kn; 897 km/h)
Range^: 36–45	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)

A Delta DC-9 with the Classic Widget Livery, 1962-1997

References

"Airliner price index". Flight International. 10 August 1972. p. 183.
"DC-9 airplane characteristics for airport planning" (PDF). Douglas aircraft company. June 1984.
"Type Certificate Data Sheet no. A6WE" (PDF). FAA. March 25, 2014. Archived from the original (PDF) on December 28, 2016. Retrieved January 12, 2019.

This article is issued from Wikipedia. The text is licensed under Creative Commons - Attribution - Sharealike. Additional terms may apply for the media files.

[1] "Airliner price index". Flight International. 10 August 1972. p. 183.

[acaps-2] "DC-9 airplane characteristics for airport planning" (PDF). Douglas aircraft company. June 1984.

[TCDS-3] "Type Certificate Data Sheet no. A6WE" (PDF). FAA. March 25, 2014. Archived from the original (PDF) on December 28, 2016. Retrieved January 12, 2019.