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UT-2L Training aircraft

UT-2L Training aircraft. First flight: 1946
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Technical specifications

DESIGNER OKB Yakovlev
COUNTRY Russia
TYPE
Training aircraft
CREW 2
POWER-PLANT One piston engine M-11D
Power, h.p. 1x145
DIMENSIONS  
Length, m 7,30
Height, m -
Wing span, m 10,50
Wing area, m2 17,00
WEIGHT  
Maximum take-off, kg -
Normal take-off, kg 950
Empty aircraft, kg -
Internal fuel, kg -
Warload, kg -
Payload, kg -
PERFORMANCE  
Maximum speed, km/h 225
Max speed in low height, km/h -
Cruising speed, km/h 200
Range, km 700
Combat range, km -
Service ceiling, m -
Rate of climb, m/min -
Maximum overload, g -
ARMAMENT Doesn't have (defensive).