Bell 222
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Re: Bell 222
Specifications
General characteristics
Crew: 4
Length: 40 ft 5 in (12.32 m)
Height: 11 ft 2 in (3.40 m)
Empty weight: 5,765 lb (2,615 kg)
Max takeoff weight: 7,485 lb (3,395 kg)
Powerplant: 2 × Avco Lycoming LTS 101-750C-1 turboshaft, 684 hp (510 kW) each
Main rotor diameter: 42 ft 0 in (12.80 m)
General characteristics
Crew: 4
Length: 40 ft 5 in (12.32 m)
Height: 11 ft 2 in (3.40 m)
Empty weight: 5,765 lb (2,615 kg)
Max takeoff weight: 7,485 lb (3,395 kg)
Powerplant: 2 × Avco Lycoming LTS 101-750C-1 turboshaft, 684 hp (510 kW) each
Main rotor diameter: 42 ft 0 in (12.80 m)
Gaillard5- Messages : 834
Re: Bell 222
Bell 230
In 1991 the 222B design was updated, given more powerful engine versions, and renamed the Bell 230. Production ended in 1995.
Bell 230 Executive
Executive transport version.
Bell 230 Utility
Utility transport version.
Bell 230 EMS
Air ambulance version, equipped with one or two stretchers.
In 1991 the 222B design was updated, given more powerful engine versions, and renamed the Bell 230. Production ended in 1995.
Bell 230 Executive
Executive transport version.
Bell 230 Utility
Utility transport version.
Bell 230 EMS
Air ambulance version, equipped with one or two stretchers.
Gaillard5- Messages : 834
Re: Bell 222
Bell 222SP
During the 1990s, some Bell 222s were modified with the 222B's engines and 230's Allison 250-C30G engines for improved single engine (engine-out) performance, and redesignated as 222SPs.
During the 1990s, some Bell 222s were modified with the 222B's engines and 230's Allison 250-C30G engines for improved single engine (engine-out) performance, and redesignated as 222SPs.
Gaillard5- Messages : 834
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