|
Wing Span |
156 feet 1 inches (47.6 m) |
|
Overall Length |
159 feet 2 inches (48.5 m) |
|
Fuselage Length |
155 feet (47.2 m) |
|
Tail Height |
52 feet (15.8 m) |
|
Body Width |
16.5 feet (5 m) |
|
Passengers |
- 181 (three-class)
- 224 (two-class)
- up to 285 (charter)
|
|
Cargo Volume |
3,070 cubic feet (86.9 cubic meters) |
|
Engines (two) |
- Pratt & Wh.tn.jpgey PW4000
- General Electric CF6-80C2
- Rolls-Royce RB211-524G/H
|
|
Maximum rated thrust per engine |
50,000 pounds to 62,000 pounds |
|
Fuel Capacity |
16,700 gallons (63,200 L) to 24,140 gallons
(91,400 L) in extended range version |
|
Maximum Takeoff Weight |
|
|
767-200 basic |
300,000 pounds (136,080 kg) |
|
767-200 max |
335,000 pounds (151,956 kg) |
|
767-200ER basic |
345,000 pounds (156,492 kg) |
|
767-200ER max |
395,000 pounds (179,172 kg) |
|
Maximum Range |
|
|
767-200 |
5,260 miles (8,465 km) |
|
767-200ER |
7,660 miles (12,330 km) |
|
Wing Span |
156 feet 1 inches (47.6 m) |
|
Overall Length |
180 feet 3 inches (54.9 m) |
|
Fuselage Length |
176 feet 1 inches (53.7 m) |
|
Tail Height |
52 feet (15.8 m) |
|
Body Width |
16.5 feet (5 m) |
|
Passengers |
- 218 (three-class)
- 269 (two-class)
- up to 325 (charter)
|
|
Cargo Volume |
4,030 cubic feet (114.2 cubic meters) |
|
Engines (two) |
- Pratt & Wh.tn.jpgey PW4000
- General Electric CF6-80C2
- Rolls-Royce RB211-524G/H
|
|
Maximum rated thrust per engine |
50,000 pounds to 62,000 pounds |
|
Fuel Capacity |
16,700 gallons (63,200 L) to 24,140 gallons
(91,400 L) in extended range version |
|
Maximum Takeoff Weight |
|
|
767-300 basic |
345,000 pounds (156,490 kg) |
|
767-300 |
351,000 pounds (159,213 kg) |
|
767-300ER basic |
380,000 pounds (172,368 kg) |
|
767-300ER max |
412,000 pounds (186,883 kg) |
|
Maximum Range |
|
|
767-300 |
4,300 miles (7,340 km) |
|
767-300ER |
6,830 miles (10,990 km) |