de Havilland Canada DHC-2 Beaver vs. PZL TS-11 Iskra

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de Havilland Canada DHC-2 Beaver versus PZL TS-11 Iskra
13.56 m 44 ft 6 in length 11.15 m 36 ft 7 in
5 m 16 ft 5 in height 3.5 m 11 ft 6 in
16.56 m 54 ft 4 in wingspan 10.06 m 33 ft
2 x Armstrong Siddeley Double Mamba turboprop engines engines 1 (WSK PZL Rzeszow SO-3W)
Approximately 3,100 hp (2,312 kW) each thrust per engine 10.8 kN
Approximately 6,200 hp (4,624 kW) total total thrust 10.8 kN
24,200 lb 10,977 kg MTOW 3,840 kg 8,466 lb
2,535 km 1,369 nm range 1,250 km 675 nm
228 mph 367 km/h cruise speed 770 km/h 478 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.