Boeing F/A-18E/F Super Hornet vs. de Havilland Canada DHC-2 Beaver

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Boeing F/A-18E/F Super Hornet versus de Havilland Canada DHC-2 Beaver
18.5 m 60 ft 3 in length 13.56 m 44 ft 6 in
4.87 m 16 ft height 5 m 16 ft 5 in
13.68 m 44 ft 1 wingspan 16.56 m 54 ft 4 in
Two F414-GE-400 turbofan engines engines 2 x Armstrong Siddeley Double Mamba turboprop engines
Up to 17,000 lbs thrust per engine Approximately 3,100 hp (2,312 kW) each
Up to 34,000 lbs total thrust Approximately 6,200 hp (4,624 kW) total
29,937 kg 66,000 lb MTOW 24,200 lb 10,977 kg
2,346 km 1,268 nm range 2,535 km 1,369 nm
1032 knots 1,911 km/h cruise speed 228 mph 367 km/h
Overall capability across all eleven hardpoints is 17,750lbs of external stores capacity Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.