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UTI-26 Training aircraft

UTI-26 Training aircraft. First flight: 1940
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Technical specifications

DESIGNER OKB Yakovlev
COUNTRY Russia
TYPE
Training aircraft
CREW 2
POWER-PLANT One piston engine M-105P
Power, h.p. 1x1.050
DIMENSIONS  
Length, m 8,48
Height, m -
Wing span, m 10,00
Wing area, m2 17,15
WEIGHT  
Maximum take-off, kg 2.750
Normal take-off, kg -
Empty aircraft, kg 2.181
Internal fuel, kg -
Warload, kg -
Payload, kg -
PERFORMANCE  
Maximum speed, km/h 586
Max speed in low height, km/h 500
Cruising speed, km/h -
Range, km 700
Combat range, km -
Service ceiling, m 9.400
Rate of climb, m/min 910
Maximum overload, g -
ARMAMENT Doesn't have (defensive).