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Bell 230 Helicopter
Duration : Twin Engined
Destination : All over India
Tour Id : BL 1996
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The Bell 230 is a twin engined max. ten seat light utility helicopter produced by the US American manufacturer Bell Helicopter Textron, produced in Mirabel, Quebec (Canada).

Crew                                                           1 / 2
Passengers                                                6 - 7, max. 9
Propulsion                                                 1 Turboshaft Engine
Engine Model                                           Allison 250-C30G2
Engine Power                        522 kW       700 shp
Speed                                   261 km/h      141 kts   162 mph
Service Ceiling                    4.724 m        15.500 ft
Range                                  520 km          281 NM 323 mi.
Empty Weight                       2.245 kg      4.950 lbs
Max. Takeoff Weight         3.810 kg        8.400 lbs
Rotor Blades (main/tail)         2/2            2/2
Main Rotor Diameter       12,8 m            42,0 ft
Tail Rotor Diameter           2,10m            6,9 ft
Rotor Disc Area               128,7m²          1385 ft²
Length (Fuselage)            12,87m            42,2 ft
Length                              15,32m            50,3 ft
Height                                3,66 m           12,0 ft
 
Remarks
The Bell 230 is a development of the Bell 222. The Bell 230 was available with retractable wheel landing gear or skid landing gear.

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