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)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.