User:Marc Lacoste/sandbox/Douglas DC-8

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	-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
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	-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
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	-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
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)

^ ^a ^b ^c ^d "Commercial Aircraft of the World" (PDF). Flight. 23 November 1961.
^ ^a ^b ^c "Airplane Characteristics for Airport Planning" (PDF). Boeing. 1989.

[Flight1961-1] "Commercial Aircraft of the World" (PDF). Flight. 23 November 1961.

[acap-2] "Airplane Characteristics for Airport Planning" (PDF). Boeing. 1989.

[1]

[2]