Specifications
| 767-200 | 767-200ER | 767-300 | 767-300ER | 767-300F | 767-400ER | |
|---|---|---|---|---|---|---|
| Cockpit crew | Two | |||||
| Seating capacity, typical |
181 (3-class) 224 (2-class) 255; optional 290 (1-class) |
218 (3-class) 269 (2-class) 350 (1-class) |
N/A | 245 (3-class) 304 (2-class) 375 (1-class) |
||
| Cargo capacity | 2,875 ft³ (81.4 m³) 22 LD2s |
3,770 ft³ (106.8 m³) 30 LD2s |
15,469 ft³ (438 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) |
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| Wingspan | 156 ft 1 in (47.6 m) |
170 ft 4 in (51.9 m) |
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| Wing area | 3,050 ft² (283.3 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) | |||||
| Maximum fuel capacity |
16,700 US gal (63,000 L) | 24,100 US gal (91,000 L) | 16,700 US gal (63,000 L) | 24,100 US gal (91,000 L) | ||
| Operating empty weight |
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 takeoff 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 |
3,850 nmi (7,300 km) transatlantic |
6,385 nmi (11,825 km) transpacific |
4,260 nmi (7,900 km) transatlantic |
5,990 nmi (11,065 km) transpacific WL: 6,310 nmi (11,690 km) |
3,255 nmi (6,025 km) transcontinental WL: 3,575 nmi (6,621 km) |
5,625 nmi (10,415 km) transpacific |
| Cruise speed | Mach 0.80 (470 knots, 530 mph, 851 km/h at 35,000 ft (11,000 m) cruise altitude) | |||||
| Maximum cruise speed |
Mach 0.86 (493 knots, 567 mph, 913 km/h at 35,000 ft (11,000 m) cruise altitude) | |||||
| Takeoff distance at MTOW (sea level, ISA) |
5,800 ft (1,768 m) | 8,300 ft (2,530 m) | 7,900 ft (2,410 m) | 8,300 ft (2,530 m) | 8,600 ft (2,621 m) | 10,200 ft (3,109 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) |
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Sources: Boeing 767 airport planning report, Boeing 767 specifications and other sources
Read more about this topic: Boeing 767