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Bell 206L4
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Bell 206L4 - Engines Rolls Royce 250-C30P HP (Takeoff) 726 SHP/541 kw
Dimensions Main Rotor 37 ft/11.3 m Tail Rotor 5.4 ft/1.7 m
Height 10.3 ft/3.1 m Length 42.4 ft/12.9 m Width 7.7 ft/2.3 m
Empty Weight 2,327 lb/1,056 kg
Max Gross Weight Std 4,450 lb/2,018 kg 
Max Gross Weight Alt n/a 
Useful Load Std 2,123 lb/962 kg Useful Load Alt n/a 
External 2,000 lb/907 kg
Vne 130 kn 241 km/h Max Cruise 112 kn 207 km/h
Max Rate of Climb 1,320 fpm 6.7 mps
HIGE 10,000 ft/3,048 m HOGE 6,500 ft/1,981 m
Service Ceiling 10,000 ft/3,048 m S/E Service Ceiling n/a
Std Fuel 110.7 gal/419 L Max Fuel n/a
IFR Crew n/a VFR Crew 1 Passengers 6
Standard Avionics None
Bell 206L4 - Engines Rolls Royce 250-C30P HP (Takeoff) 726 SHP/541 kw Dimensions Main Rotor 37 ft/11.3 m Tail Rotor 5.4 ft/1.7 m Height 10.3 ft/3.1 m Length 42.4 ft/12.9 m Width 7.7 ft/2.3 m Empty Weight 2,327 lb/1,056 kg Max Gross Weight Std 4,450 lb/2,018 kg Max Gross Weight Alt n/a Useful Load Std 2,123 lb/962 kg Useful Load Alt n/a External 2,000 lb/907 kg Vne 130 kn 241 km/h Max Cruise 112 kn 207 km/h Max Rate of Climb 1,320 fpm 6.7 mps HIGE 10,000 ft/3,048 m HOGE 6,500 ft/1,981 m Service Ceiling 10,000 ft/3,048 m S/E Service Ceiling n/a Std Fuel 110.7 gal/419 L Max Fuel n/a IFR Crew n/a VFR Crew 1 Passengers 6 Standard Avionics None
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