Engine:
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Vedeneyev M-14P 360 hp (269 kW) 9 cylinder aircooled radial
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Propeller
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Two-blade variable pitch wooden V-530TA-D35 |
Dimensions:
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Span
Length
Height
Wings area
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9,5 m
7,67 m
2,7 m
15,0 m2
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31,1 ft
25,1 ft
8,9 ft
161,2 ft2
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Weights and loadings:
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Basic empty weight
Maximum takeoff weight
Basic fuel capacity
Max wing loading
Max wing loading
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765 kg
900 kg
95 kg
60 kg /m2
2,5 kg/hp
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1687 lb
2951 lb
209 lb
12,3 lb/ft2
10,8 lb/kW
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Performances:
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Maximum level speed @ 1000 m
Vne
Landing speed
Maximum rate of climb
Service ceiling
Maximum range (10 % reserve)
Maximum endurance
Take off run (sea level)
Landing run (sea level)
Maximum load factor
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300 km/h
360 km/h
110 km/h
16 m/s
4000 m
500 km
2,6 hr
200 m
250 m
+ 9 / - 6
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162 mph
194 mph
59 mph
3148 fpm
13115 ft
270 nm
2,6 hr
655 ft
820 ft
+ 9 / - 6
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