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The SM-2, a Polish development of the basic design was flown late in 1959. This has a longer nose, thereby enlarging the cabin to accommodate 4 passengers in addition to the pilot. In the ambulance role, the SM-2 can take a third stretcher inside the cabin in addition to the two carried on external panniers. Production of the SM-2 was initiated in 1961 to fulfil both military and civil orders. K.Munson "Helicopters And Other Rotorcraft Since 1907", 1968
Technical data for PZL Swidnik SM-2
Engine: 1 x Lit-3 pistone engine, rated at 425kW,
main rotor diameter: 14.3m,
length: 17.0m,
height: 3.1m,
take-off weight: 2550kg,
empty weight: 1934kg,
max speed: 170km/h,
cruising speed: 130km/h,
ceiling: 3700m,
range with max fuel: 550km
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Stack trace:
#0 /data03/virt15346/domeenid/www.aviastar.org/htdocs/helicopters_eng/pzl_sm-2.php(71): mysqli_connect('mysql5.zone.ee', 'd14657sa18989', Object(SensitiveParameterValue))
#1 {main}
thrown in /data03/virt15346/domeenid/www.aviastar.org/htdocs/helicopters_eng/pzl_sm-2.php on line 71
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