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Two-seat liaison machine developed from A-6 and A-8. Direct-control inclined rotor with folding blades, folding dihedralled wings and twin-finned tail, internal engine starter and clutch-in drive for rotor before take-off. First flown on skis March 1936. Bill Gunston "The Osprey's Encyclopedia of Russian Aircraft", 2000
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| Technical data for A-13
Engine: 1 x M-11,
rotor diameter: 11.5m,
wing area: 5.6m2,
weight empty: 540kg,
fuel+oil: 50kg,
weight loaded: 802kg,
max speed: 151km/h,
min speed: 45km/h,
ceiling: 3000m,
endurance: 2h,
range: 250km,
take-off run: 40m,
landing run: 0m
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