Pt En

Range

Economical Cruising, MTOW, 4,000 ft, ISA, No Auxiliary Tank, No Fuel Reserve

365 NM / 676 km

Maximum Cruising Speed

4,500 lb, 4,000 ft, ISA+20°C

141 ktas / 261 km/h

Engine

Rolls-Royce M250-C47E/4

862 shp

Number of Seats

Pilots + Passengers

1+6 or 2+5

Maximum Takeoff Weight

5,250 lb / 2,381 kg

Payload

1,160 kg

Avionics

Garmin
G1000H NXi

MAIN DIFFERENCES

PERFORMANCE

The Bell 407GXi is equipped with a new Rolls-Royce engine, with more take-off power and at the same time, lower fuel consumption. The model also features a FADEC system, Full-Full takeoff (full fuel, full pax and cargo) and excellent performance in tropical climates.
Economia

COST SAVINGS

The Bell 407GXi is the helicopter that goes further when it comes to cost savings. In addition to lower fuel consumption, the aircraft features the extension of the general transmission overhaul, which ensures the reduction of maintenance costs and increases the machine's availability from 4,500 to 5,000 hours.

TECHNOLOGY

At the forefront of the segment, the Bell 407GXi was the first helicopter equipped with the Glass Cockpit Garmin G1000H panel with SVT, which is even more intuitive and offers better performance. The model also features composite blades, a video camera for the tail rotor, as well as other features that make its operation even safer.
Tecnologia
DESIGN
The model has bold and well defined lines, which translate to product excellence.
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IMAGE GALLERY
INTERIOR SPACE
The Bell 407GXi features ample and comfortable seating that accommodates up to six passengers.
DETAILED SPECIFICATIONS
DIMENSIONS
Length 12.61 m
Height 3.30 m
Engine Diameter 10.66 m

CABIN
Seats (pil. + pass.) 1+6 or 2+5
   
WEIGHTS
Maximum Takeoff Weight 5,250 lb (2,381 kg)
Payload 1,160 kg
Maximum Fuel 147 gal (556 L)
   
LUGGAGE CAPACITY
Total Volume 0.45 m3
   
   
PERFORMANCE
Maximum Range1 365 NM (676 km)
Max. Cruising Speed2 141 ktas (261 km/h)
   
EQUIPMENT  
Engine
  Rolls-Royce M250-C47E/4
Avionics

Garmin G1000H NXi

1 Economical Cruising, MTOW, 4,000 ft, ISA, No Auxiliary Tank, No Fuel Reserve;  
2 4,000 ft, ISA+20°C.

 
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