Boeing 767: Difference between revisions
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m Protected "Boeing 767" [edit=autoconfirmed:move=autoconfirmed] |
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Latest revision as of 18:26, 24 December 2009
| Boeing 767 at a Glance | |
|---|---|
| Role | Widebody Jetliner |
| Country of Origin | United States |
| Manufacturer | Boeing |
| Status | In Production |
| Number Built | 977 |
| Unit Cost | 80,000,000-139,000,000 |
| File:Airplanes-Boeing 767.jpg | |
767-200
767-200ER
767-200ERF
767-300
767-300ER
767-300F
767-400ER
Specifications
Specifications
| 767-200 | 767-200ER | 767-300 | 767-300ER | 767-300F | 767-400ER | |
|---|---|---|---|---|---|---|
| Cockpit crew | Two | |||||
| Passengers | 181 (3 class) 224 (2 class) 255 optional 290 (1 class) |
218 (3 class) 269 (2 class) 350 (1 class) |
- | 245 (3 class) 304 (2 class) 375 (1 class) | ||
| Cargo | 2,875 ft³ (81.4 m³) 22 LD2s |
3,770 ft³ (106.8 m³) 30 LD2s |
16,034 ft³ (454 m³) 30 LD2s + 24 pallets |
4,580 ft³ (129.6 m³) 38 LD2s | ||
| Length | 159 ft 2 in (48.5 m) |
180 ft 3 in (54.9 m) |
201 ft 4 in (61.4 m) | |||
| Wingspan | 156 ft 1 in (47.6 m) |
170 ft 4 in (51.9 m) | ||||
| Wing area | 3,050 ft² (283.3 sq m²) | 3,130 ft ² (290.7 m²) | ||||
| Fuselage height | 17 ft 9 in (5.41 m) | |||||
| Fuselage width | 16 ft 6 in (5.03 m) | |||||
| Cabin width (interior) | 15 ft 6 in (4.72 m) | |||||
| Empty Weight, operating |
176,650 lb (80,130 kg) |
181,610 lb (82,380 kg) |
189,750 lb (86,070 kg) |
198,440 lb (90,010 kg) |
190,000 lb (86,180 kg) |
229,000 lb (103,870 kg) |
| Maximum take-off weight | 315,000 lb (142,880 kg) |
395,000 lb (179,170 kg) |
350,000 lb (158,760 kg) |
412,000 lb (186,880 kg) |
412,000 lb (186,880 kg) |
450,000 lb (204,120 kg) |
| Maximum Range at MTOW |
3,950 NM (7,300 km) transatlantic |
6,590 NM (12,200 km) transpacific |
3,950 NM (7,300 km) transatlantic |
5,975 NM (11,065 km) transpacific |
3,255 NM (6,025 km) transcontinental |
5,625 NM (10,415 km) transpacific |
| Cruise speed | Mach 0.80 (470 kn, 530 mph, 851 km/h at 35,000 ft cruise altitude) | |||||
| Max. Cruise speed | Mach 0.86 (493 kn, 568 mph, 913 km/h at 35,000 ft cruise altitude) | |||||
| Takeoff run at MTOW |
5,600 ft (1,710 m) | 7,900 ft (2,410 m) | 9,501 ft (2,896 m) | |||
| Engines (x2) | P&W JT9D-7R4 P&W PW4000-94 GE CF6-80A GE CF6-80C2 |
P&W PW4000-94 GE CF6-80C2 |
P&W JT9D-7R4 P&W PW4000-94 GE CF6-80A GE CF6-80C2 |
P&W PW4000-94 GE CF6-80C2 RR RB211-524H |
P&W PW4000-94 GE CF6-80C2 | |
| Thrust (x2) | GE: 50,000 lbf (222 kN) | PW: 63,300 lb (282 kN) GE: 62,100 lbf (276 kN) |
PW: 50,000 lbf (220 kN) | PW: 63,300 lbf (282 kN) GE: 62,100 lbf (276 kN) RR: 59,500 lbf (265 kN) |
PW: 63,300 lbf (282 kN) GE: 63,500 lbf (282 kN) | |