Boeing B767-338 ER Australian Airlines VH-OGJ at Taxiway D
Boeing B767-338 ER Australian Airlines VH-OGJ in profile
| 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) 290; optional 350 (1-class) |
N/A | 245 (3-class) 304 (2-class) 409 (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) |
|||
| Wingspan | 156 ft 1 in (47.6 m) |
170 ft 4 in (51.9 m) |
||||
| Wing area | 3,050 ft² (283.3 m²) | 3,130 ft² (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) | 24,140 US gal (91,400 L) | 16,700 US gal (63,000 L) | 24,140 US gal (91,400 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 (4,430 mi; 7,130 km) | 6,385 nmi (7,348 mi; 11,825 km) | 4,260 nmi (4,900 mi; 7,890 km) | 5,990 nmi (6,890 mi; 11,090 km) WL: 6,310 nmi (7,260 mi; 11,690 km) |
3,255 nmi (3,746 mi; 6,028 km) WL: 3,575 nmi (4,114 mi; 6,621 km) |
5,625 nmi (6,473 mi; 10,418 km) |
| 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 PW4052 GE CF6-80A, A2, or C2 |
P&W PW4052, or 4056 GE CF6-80C2 RR RB211-524G or H |
P&W JT9D-7R4 P&W PW4052 GE CF6-80A, or C2 RR RB211-524H |
P&W PW4056, 4060, or 4062 GE CF6-80C2 RR RB211-524G, or H |
P&W PW4062 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) |
|
© 2004-2024 Aeronautic pictures. This website, the content, the design and the pictures and are intended for public non commercial use, and may be redistributed, freely printed, or electronically reproduced in its complete and unaltered form provided distribution is for private use only. Partial and other distribution means require the permission of Aeronautic Pictures. All rights reserved.