Bell 407

General characteristics:

Crew: 1–2 pilots 
Passenger capacity: up to 6 passengers 
Payload: 1,178 kg 
Length: 12.74 m 
Fuselage length: 10.58 m 
Main rotor diameter: 10.67 m 
Tail rotor diameter: 1.65 m 
Fuselage width : 2.29 m (on runners) 
Height: 3.32 m 
Area swept by the main rotor: 89.38 m² 
Empty weight: 1,203 kg 
Normal takeoff weight: 2,268 kg 
Maximum takeoff weight: 2,381 kg 
with suspension: 2,721 kg 
Volume of fuel tanks: 484 l (+ 72 l in the luggage compartment) 
Power source: 1 × Rolls-Royce 250-C47B turboshaft 
Engine power: 1 × 760 hp 
(1 × 606 kW (takeoff)) 

Dimensions of the cargo compartment: 

Width: 1.37 m 
Height: 1.0 m 

Flight characteristics 

Maximum permissible speed: 259 km / h 
Maximum speed: 
at the ground: 246 km / h 
at an altitude of 1 220 m : 250 km / h 
Cruising speed: 
at the ground: 207 km / h 
at an altitude of 1 220 m: 213 km / h 
Practical range: 611 km 
Flight duration: 3 hours 42 minutes. 
Service ceiling: 6,100 m 

Static ceiling: 
ground effect: 3 720 m 
without ground effect: 3,170 m 
Rate of climb: 6.8 m / s 
Disc load: 27.9 kg / m² 
Thrust-to- weight ratio: 221 W / kg ( for transmission at normal takeoff weight)