Boeing 767-400ER vs. Lockheed U-2
... or view the full comparison list
here.
Boeing 767-400ER |
versus |
Lockheed U-2 |
61.3 m |
201 ft 3 in |
length |
19.2 m |
63 ft 0 in |
16.9 m |
55 ft 5 in |
height |
4.8 m |
15 ft 9 in |
51.9 m |
170 ft 3 in |
wingspan |
32 m |
105 ft |
2 Pratt & Whitney PW4060 turbofan engines |
engines |
1 × General Electric F118-101 |
Up to 63,300 pounds |
thrust per engine |
17,000 lbf (76 kN) |
Up to 126,600 pounds |
total thrust |
17,000 lbf (76 kN) |
204,120 kg |
450,100 lb |
MTOW |
18,144 kg |
40,000 lb |
9,688 km |
5,232 nm |
range |
6,090 nm |
11,278 km |
530 mph |
853 km/h |
cruise speed |
475 mph |
764 km/h |
Typical three class arrangement for 245 passengers |
capacity |
|
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.