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Agusta-Bell 47G-3B-2

Agusta-Bell 47G-3B-2. First flight: 1966 © Marcos Andreou
Photo archive M. Andreou

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It is one light single seat, single-engine helicopter with a Lycoming VO-540-B1B3 piston engine with a power of 308 hp. The first flight was made in 1966. All helicopters were joined to the 359th Squadron (Public Services Air Support) and were used mainly in agricultural work (spraying, spraying liquid / dry chemicals, etc.). All helicopters have been decommissioned from the Hellenic Air Force. 

 

Patches

359 Public Services Air Support Unit 359 Public Services Air Support Unit

 

 


Technical specifications

DESIGNER
Agusta - Bell
COUNTRY
USA, Italy
TYPE
Multipurpose helicopter
CREW
1
POWER-PLANT
One Lycoming VO-540-B1B3
Power, h.p. 1x308 (284)
DIMENSIONS
 
Length, m
9,90
Main rotor diameter , m
11,32
Tail rotor diameter, m
1,78
Height, m
2,72
WEIGHT  
Maximum take-off, kg 1.338
Normal take-off, kg -
Empty aircraft, kg 827
Internal fuel, l 216
Payload, kg  
- passengers 2
PERFORMANCE
 
Maximum speed, km/h
169
Cruising speed, km/h
143
Economic speed, km/h -
Rate of climb, m/min
244
Service ceiling, m
3.415
Static ceiling, m
2.345
Range, km -
Combat range, km -
ARMAMENT Doesn't have (defensive).





Photos Agusta-Bell 47G-3B-2