Boeing 767-200ER vs. Northrop T-38 Talon

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Boeing 767-200ER versus Northrop T-38 Talon
48.5 m 159 ft 2 in length 14.1 m 46 ft 4 in
16.1 m 52 ft 10 in height 3.9 m 12 ft 10 in
47.8 m 156 ft 9 in wingspan 7.7 m 25 ft 3 in
2 x GE CF6-80C2B4F engines Two General Electric J85-GE-5A turbojet engines
62,020 lbs thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
124,040 lbs total thrust 4,100 pounds dry thrust; 5,800 with afterburners
164,200 kg 362,000 lb MTOW 12,093 lb 5,485 kg
12,200 km 6,587 nmi range 1,759 km 950 nm
850 km/hour 528 mph cruise speed 745 kts 1,380 km/h
249 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.