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Robinson R22 Two-seat light helicopter

Robinson R22 Two-seat light helicopter. First flight: 1975 © Μ. Ανδρέου
Photo archive K. Panitsidi & M. Andreou

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Technical specifications

DESIGNER Robinson
COUNTRY USA
TYPE Two-seat light helicopter
CREW 2
POWER-PLANT One Textron Lycoming O-320-B2C engine
Power, h.p. 1x162
DIMENSIONS
 
Length, m
6,30
Fuselage length, m
-
Main rotor diameter, m
7,67
Tail rotor diameter, m
1,07
Height, m
2,67
WEIGHT  
Maximum take-off, kg 621
Normal take-off, kg -
Empty, kg 379
Internal fuel, l 52
- + optionally 29
Payload, kg -
PERFORMANCE  
Maximum speed, km/h 190
Cruising speed, km/h
180
Economic speed, km/h
-
Maximum overload, g
-
Rate of climb, m/min
366
Service ceiling, m
4.265
Static ceiling, m
2.125
Range, km
592
Combat range, km
-
Endurance, h
-
ARMAMENT Doesn't have (defensive).





Photos Robinson R22