FIELD: aviation. SUBSTANCE: cargo handling system has longitudinal control handle 2 mounted in suspended pilot's cockpit 1 and handles 8 and 9 mounted in main pilot's cockpit. Handles 1, 8 and 9 are engaged via linkages 3 and 4 with plate 5 of helicopter rotor swash plate 6 whose fuselage 7 is provided with door 15. Handle 2 is spaced from the longitudinal plane of symmetry of helicopter fuselage 7 the distance equal to 0.2-0.6 the fuselage maximum diameter and the distance from handle 2 to fuselage nose 7 is equal to 0.08-0.15 the fuselage length. EFFECT: more convenient cargo handling in case of expansion of helicopter fleet. 6 dwg
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