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User:Marc Lacoste/sandbox/Douglas DC-8

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Four columns

[edit]
DC-8-10/20/30/40/50,[1] DC-8-43/55/61/62/63/71/72/73[2]
Variant -10/20/30 -40/43/50/55 -61/63/71/73 -62/72
Passengers 177 -40/43: 177
-50/55: 189
259 189
Max. cargo 1,390 cu ft (39 m3) 2,500 cu ft (71 m3) 1,615 cu ft (45.7 m3)
Wingspan 142.4 ft (43.4 m) -61/71: 142.4 ft (43.4 m)
-63/73: 148.4 ft (45.2 m)
148.4 ft (45.2 m)
Length 150.7 ft (45.9 m) 187.4 ft (57.1 m) 157.5 ft (48.0 m)
Fuselage outside width: 147 in (373.4 cm), inside width: 138.25 in (351.2 cm)
MTOW -10: 273,000 lb (123.8 t)
-20: 276,000 lb (125.2 t)
30: 315,000 lb (142.9 t)
315,000 lb (142.9 t)
-55: 325,000 lb (147.4 t)
-61/71: 325,000 lb (147.4 t)
-61F/71F: 328,000 lb (148.8 t)
-63/73: 355,000 lb (161.0 t)
350,000 lb (158.8 t)
-72F : 335,000 lb (152.0 t)
Max PL -10: 46,103 lb (20.9 t)
-20: 43,624 lb (19.8 t)
-30: 51,870 lb (23.5 t)
52,000 lb (23.6 t)
-43: 41,691 lb (18.9 t)
-61: 71,899 lb (32.6 t)
-71: 60,300 lb (27.4 t)
-63: 71,262 lb (32.3 t)
-73: 64,800 lb (29.4 t)
-62: 51,745 lb (23.5 t)
-72: 41,800 lb (19.0 t)
OEW -10: 119,797 lb (54.3 t)
-20: 123,876 lb (56.2 t)
-30: 126,330 lb (57.3 t)
-40/50: 124,800 lb (56.6 t)
-43: 136,509 lb (61.9 t)
-55: 138,266 lb (62.7 t)
-61: 152,101 lb (69.0 t)
-71: 163,700 lb (74.3 t)
-63: 158,738 lb (72.0 t)
-73: 166,200 lb (75.4 t)
-62: 143,255 lb (65.0 t)
-72: 153,200 lb (69.5 t)
max fuel -10/20: 17,550 US gal (66.4 m3)
-30: 23,393 US gal (88.6 m3)
23,393 US gal (88.6 m3) -61/71: 23,393 US gal (88.6 m3)
-63/73: 24,275 US gal (91.9 m3)
24,275 US gal (91.9 m3)
Turbojets -10: P&W JT3C
-20/30: P&W JT4A
-40/43: RCo.12
-50/55: P&W JT3D-3
super 60: P&W JT3D-3B
super 70: CFM56-2
Turbofans
Cruise Mach 0.82 (483 kn; 895 km/h)
Range -10: 3,760 nmi (6,960 km)
-20: 4,050 nmi (7,500 km)
-30: 4,005 nmi (7,417 km)
-40: 5,310 nmi (9,830 km)
-43: 4,200 nmi (7,800 km)
-50: 5,855 nmi (10,843 km)
-55: 4,700 nmi (8,700 km)
-61: 3,200 nmi (5,900 km)
-71: 3,500 nmi (6,500 km)
-63: 4,000 nmi (7,400 km)
-73: 4,500 nmi (8,300 km)
-62: 5,200 nmi (9,600 km)
-72: 5,300 nmi (9,800 km)
Freighters -50/-55 -61/71/63/73 -62/72
Volume -50: 9,310 cu ft (264 m3)
-55: 9,020 cu ft (255 m3)
-61/71: 12,171 cu ft (344.6 m3)
-63/73: 12,830 cu ft (363 m3)
9,737 cu ft (275.7 m3)
Payload -50: 88,022 lb (39.9 t)
-55: 92,770 lb (42.1 t)
-61: 88,494 lb (40.1 t)
-71: 81,300 lb (36.9 t)
-63: 119,670 lb (54.3 t)
-73: 111,800 lb (50.7 t)
-62: 91,440 lb (41.5 t)
-72: 90,800 lb (41.2 t)
OEW -50: 130,207 lb (59.1 t)
-55: 131,230 lb (59.5 t)
-61: 145,506 lb (66.0 t)
-71: 152,700 lb (69.3 t)
-63: 141,330 lb (64.1 t)
-73: 149,200 lb (67.7 t)
-62: 138,560 lb (62.8 t)
-72: 140,200 lb (63.6 t)
Range -55: 3,000 nmi (5,600 km) -61/63: 2,300 nmi (4,300 km)
-71/73: 2,900 nmi (5,400 km)
-62: 3,200 nmi (5,900 km)
-72: 3,900 nmi (7,200 km)

Five columns

[edit]
DC-8-10/20/30/40/50,[1] DC-8-43/55/61/62/63/71/72/73[2]
Variant -10/20/30 -40/43/50/55 -61/71 -63/73 -62/72
Passengers 177 -40/43: 177
-50/55: 189
259 189
Max. cargo 1,390 cu ft (39 m3) 2,500 cu ft (71 m3) 1,615 cu ft (45.7 m3)
Wingspan 142.4 ft (43.4 m) 148.4 ft (45.2 m)
Length 150.7 ft (45.9 m) 187.4 ft (57.1 m) 157.5 ft (48.0 m)
Fuselage outside width: 147 in (373.4 cm), inside width: 138.25 in (351.2 cm)
MTOW -10: 273,000 lb (123.8 t)
-20: 276,000 lb (125.2 t)
30: 315,000 lb (142.9 t)
315,000 lb (142.9 t)
-55: 325,000 lb (147.4 t)
325,000 lb (147.4 t)
-F: 328,000 lb (148.8 t)
355,000 lb (161.0 t) 350,000 lb (158.8 t)
-72F : 335,000 lb (152.0 t)
Max PL -10: 46,103 lb (20.9 t)
-20: 43,624 lb (19.8 t)
-30: 51,870 lb (23.5 t)
52,000 lb (23.6 t)
-43: 41,691 lb (18.9 t)
-61: 71,899 lb (32.6 t)
-71: 60,300 lb (27.4 t)
-63: 71,262 lb (32.3 t)
-73: 64,800 lb (29.4 t)
-62: 51,745 lb (23.5 t)
-72: 41,800 lb (19.0 t)
OEW -10: 119,797 lb (54.3 t)
-20: 123,876 lb (56.2 t)
-30: 126,330 lb (57.3 t)
-40/50: 124,800 lb (56.6 t)
-43: 136,509 lb (61.9 t)
-55: 138,266 lb (62.7 t)
-61: 152,101 lb (69.0 t)
-71: 163,700 lb (74.3 t)
-63: 158,738 lb (72.0 t)
-73: 166,200 lb (75.4 t)
-62: 143,255 lb (65.0 t)
-72: 153,200 lb (69.5 t)
max fuel 23,393 US gal (88.6 m3)
-10/20: 17,550 US gal (66.4 m3)
24,275 US gal (91.9 m3)
Turbojets -10: P&W JT3C
-20/30: P&W JT4A
-40/43: RCo.12
-50/55: P&W JT3D-3
super 60: P&W JT3D-3B
super 70: CFM56-2
Turbofans
Cruise Mach 0.82 (483 kn; 895 km/h)
Range -10: 3,760 nmi (6,960 km)
-20: 4,050 nmi (7,500 km)
-30: 4,005 nmi (7,417 km)
-40: 5,310 nmi (9,830 km)
-43: 4,200 nmi (7,800 km)
-50: 5,855 nmi (10,843 km)
-55: 4,700 nmi (8,700 km)
-61: 3,200 nmi (5,900 km)
-71: 3,500 nmi (6,500 km)
-63: 4,000 nmi (7,400 km)
-73: 4,500 nmi (8,300 km)
-62: 5,200 nmi (9,600 km)
-72: 5,300 nmi (9,800 km)
Freighters -50/-55 -61/71 63/73 -62/72
Volume -50: 9,310 cu ft (264 m3)
-55: 9,020 cu ft (255 m3)
12,171 cu ft (344.6 m3) 12,830 cu ft (363 m3) 9,737 cu ft (275.7 m3)
Payload -50: 88,022 lb (39.9 t)
-55: 92,770 lb (42.1 t)
-61: 88,494 lb (40.1 t)
-71: 81,300 lb (36.9 t)
-63: 119,670 lb (54.3 t)
-73: 111,800 lb (50.7 t)
-62: 91,440 lb (41.5 t)
-72: 90,800 lb (41.2 t)
OEW -50: 130,207 lb (59.1 t)
-55: 131,230 lb (59.5 t)
-61: 145,506 lb (66.0 t)
-71: 152,700 lb (69.3 t)
-63: 141,330 lb (64.1 t)
-73: 149,200 lb (67.7 t)
-62: 138,560 lb (62.8 t)
-72: 140,200 lb (63.6 t)
Range -55: 3,000 nmi (5,600 km) -61/63: 2,300 nmi (4,300 km)
-71/73: 2,900 nmi (5,400 km)
-62: 3,200 nmi (5,900 km)
-72: 3,900 nmi (7,200 km)

Imperial units

[edit]
DC-8-10/20/30/40/50,[1] DC-8-43/55/61/62/63/71/72/73[2]
Variant -10/20/30 -40/43/50/55 -61/71 -63/73 -62/72
Passengers 177 -40/43: 177
-50/55: 189
259 189
Max. cargo 1,390 cu ft 2,500 cu ft 1,615 cu ft
Wingspan 142.4 ft 148.4 ft
Length 150.7 ft 187.4 ft 157.5 ft
Fuselage outside width: 147 in (373.4 cm), inside width: 138.25 in (351.2 cm)
MTOW (lb) -10: 273,000
-20: 276,000
30: 315,000
315,000
-55: 325,000
325,000
-F: 328,000
355,000 350,000
-72F : 335,000
Max PL (lb) -10: 46103
-20: 43624
-30: 51870
52000
-43: 41691
-61: 71899
-71: 60300
-63: 71262
-73: 64800
-62: 51745
-72: 41800
OEW (lb) -10: 119,797
-20: 123,876
-30: 126,330
-40/50: 124,800
-43: 136,509
-55: 138,266
-61: 152,101
-71: 163,700
-63: 158,738
-73: 166,200
-62: 143,255
-72: 153,200
max fuel 23,393 US gal (-10/20: 17,550 US gal) 24,275 US gal
Turbojets -10: P&W JT3C
-20/30: P&W JT4A
-40/43: RCo.12
-50/55: P&W JT3D-3
super 60: P&W JT3D-3B
super 70: CFM56-2
Turbofans
Cruise Mach 0.82 (483 kn; 895 km/h)
Range (nmi) -10: 3,760
-20: 4,050
-30: 4,005
-40: 5,310
-43: 4,200
-50: 5,855
-55: 4,700
-61: 3,200
-71: 3,500
-63: 4,000
-73: 4,500
-62: 5,200
-72: 5,300
Freighters -50/-55 -61/71 63/73 -62/72
Volume -50: 9310 cu ft
-55: 9,020 cu ft
12,171 cu ft 12,830 cu ft 9,737 cu ft
Payload (lb) -50: 88,022
-55: 92,770
-61: 88,494
-71: 81,300
-63: 119,670
-73: 111,800
-62: 91,440
-72: 90,800
OEW (lb) -50: 130,207
-55: 131,230
-61: 145,506
-71: 152,700
-63: 141,330
-73: 149,200
-62: 138,560
-72: 140,200
Range (nmi) -55: 3,000 -61/63: 2,300
-71/73: 2,900
-62: 3,200
-72: 3,900

Extra Specifications

[edit]
DC-8-10/20/30/40/50/8F Extra Specifications[1]
Variant DC-8-10 DC-8-20 DC-8-30 DC-8-40 DC-8-50 DC-8F
Seat pitch 32-35 in 28 in
Cabin length 103 feet 5 inches (31.52 m)
Height, overall 42 ft 4 in (12.90 m)
Wing area 2,725 sq ft
253.2 m2
2,883.6 sq ft
267.90 m2
sweepback 30°
Payload 37,315 lb
16,926 kg
35,443 lb
16,077 kg
41,645 lb
18,890 kg
88,022 lb
39,926 kg
Thrust 4×13,500 lbf (60 kN) 4×15,800–16,800 lbf (70–75 kN) 4×15,800–17,500 lbf (70–78 kN) 4×18,000 lbf (80 kN)
SFC 0.0420 nmi/lb (0.171 km/kg)
Altitude, typical 35,000 ft (11,000 m)
Take-off distance, typical 9,550 ft (2,910 m) 7,100 ft (2,200 m) 9,620 ft (2,930 m) 9,050 ft (2,760 m) 9,300 ft (2,800 m)
Max. landing distance 6,410 ft (1,950 m) 6,800 ft (2,100 m) 6,555 ft (1,998 m) 7,450 ft (2,270 m)
Range at max. fuel 4,067 nmi (4,680 mi; 7,532 km) 4,425 nmi (5,092 mi; 8,195 km) 5,250 nmi (6,040 mi; 9,720 km) 5,905 nmi (6,795 mi; 10,936 km) 6,550 nmi (7,540 mi; 12,130 km)
Payload at max. fuel 27,840 lb
12,630 kg
26,600 lb
12,100 kg
25,475 lb
11,555 kg
23,375 lb
10,603 kg
25,915 lb
11,755 kg
28,830 lb
13,080 kg
VNE 390 kn (450 mph; 720 km/h)
VNO 340–376 kn (391–433 mph; 630–696 km/h) 340–374 kn (391–430 mph; 630–693 km/h)
Vso 133 kn (153 mph; 246 km/h) 136 kn (157 mph; 252 km/h) 147 kn (169 mph; 272 km/h)
VSF 103 kn (119 mph; 191 km/h) 107 kn (123 mph; 198 km/h) 115 kn (132 mph; 213 km/h)
  1. ^ a b c d "Commercial Aircraft of the World" (PDF). Flight. 23 November 1961.
  2. ^ a b c "Airplane Characteristics for Airport Planning" (PDF). Boeing. 1989.