User:Marc Lacoste/sandbox/Douglas DC-8
Four columns
[edit]| 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]| 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]| 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]| 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.