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Boeing B767-238ER
GENERAL INFORMATION
| Cockpit Crew |
2 |
| Capacity |
Business Class:60 / Economy Class: 90 |
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| Engines (x2) |
Pratt & Whitney JT9D-7R4E |
| Maximum Taxi Weight |
322,000 lbs |
| Maximum Gross Weight Take-Off |
320,000 lbs |
| Maximum Landing Weight |
278,000 lbs |
| Empty Operating Weight |
178,087 lbs |
| Maximum Zero Fuel Weight |
253,000 lbs |
| Maximum Fuel Capacity |
20,450 gals US |
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| Cruise Speed |
Mach 0.80 (470 kts, 530 mph, 851km/h at 35,000 ft cruise
altitude |
| Maximum Cruise Speed |
Mach 0.86 (493 kts, 568 mph, 913 km/h at 35,000 cruise
altitude) |
| Maximum Range at MTOW |
900 nm |
| Take-Off Run at MTOW |
5,600 ft / 1n710 m |
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Overall
Dimensions |
| Length |
159 ft 2 in |
| Wing Span |
156 ft 1 in / 47.6 m |
| Wing Area |
3,050 ft² / 283.3 m² |
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Cabin
Dimensions |
| Cabin Width (Interior) |
15 ft 6 in / 4.72 m |
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* This data is for general information only and subject to
verification. All performance data assumes ISA conditions. |
