Boeing 767-400ER vs. Northrop T-38 Talon
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Boeing 767-400ER |
versus |
Northrop T-38 Talon |
61.3 m |
201 ft 3 in |
length |
14.1 m |
46 ft 4 in |
16.9 m |
55 ft 5 in |
height |
3.9 m |
12 ft 10 in |
51.9 m |
170 ft 3 in |
wingspan |
7.7 m |
25 ft 3 in |
2 Pratt & Whitney PW4060 turbofan engines |
engines |
Two General Electric J85-GE-5A turbojet engines |
Up to 63,300 pounds |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
Up to 126,600 pounds |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
204,120 kg |
450,100 lb |
MTOW |
12,093 lb |
5,485 kg |
9,688 km |
5,232 nm |
range |
1,759 km |
950 nm |
530 mph |
853 km/h |
cruise speed |
745 kts |
1,380 km/h |
Typical three class arrangement for 245 passengers |
capacity |
Two (student and instructor) |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.