Bell 407GXi

The Bell 407GXi is a seven-seat, single-engine helicopter designed for corporate transport, public safety, emergency medical service, utility, training and special-mission operations. It combines the Bell 407 family’s four-blade rotor system and adaptable cabin with a Rolls-Royce 250-C47E/4 engine, dual-channel digital engine control and Garmin G1000H NXi avionics.

ManufacturerBell
StatusCurrent
Country of originCanada

Primary roles: Corporate transport, public safety, utility, helicopter emergency medical services, search and rescue, training and special missions

Configuration: Single main rotor

Overview

The Bell 407GXi is the current production version of Bell’s 407 light-single helicopter family. The aircraft combines seating for one pilot and six passengers with a cabin that can be configured for corporate transportation, public safety, emergency medical service, utility work, training and other specialized missions.

Its powerplant is a Rolls-Royce 250-C47E/4 turboshaft equipped with dual-channel full-authority digital engine control, commonly known as FADEC. Bell lists the engine at 862 shaft horsepower for takeoff and 761 shaft horsepower at maximum continuous power. The digital control system manages engine operation while reducing the number of manual power-management tasks required of the pilot.

Cockpit and avionics

The 407GXi introduced the Garmin G1000H NXi integrated flight deck to the Bell 407 series. Its features include high-resolution displays, synthetic vision, terrain-awareness functions, flight planning, fuel-flow information and range-ring mapping. Optional and supplemental systems can add traffic information, weather data, wire-awareness functions and other mission capabilities.

Bell announced the 407GXi in 2018 as an advancement of the earlier 407GX and 407GXP. The updated model paired the newer avionics suite with the Rolls-Royce 250-C47E/4 engine and dual-channel FADEC. Transport Canada certified the aircraft in 2018, followed by FAA validation later that year.

Performance and missions

Bell publishes a maximum cruise speed of 133 knots and a range of 337 nautical miles under stated standard conditions with no reserve. Standard seating accommodates one pilot and six passengers. The base aircraft has a standard internal useful load of 2,300 pounds, while optional configurations can raise internal maximum gross weight and useful load.

The 407GXi’s adaptable cabin and external-load capability allow the same basic aircraft family to serve markedly different operators. Examples include law-enforcement agencies, emergency medical providers, corporate flight departments, utility operators and military or government organizations.

Specifications and performance can vary by equipment, configuration, environmental conditions and approved operating limitations. Operational decisions must always rely on the applicable rotorcraft flight manual and current approved documentation.

The avionics and engine descriptions are supported by Bell’s current product information and its GXi launch announcement. Bell product specifications, Bell launch announcement

Specifications

Figures can vary by variant, configuration and operating conditions. Consult approved manufacturer documentation for operational use.

Entered service
2018
Production
2018–present
Engine configuration
1 × Rolls-Royce 250-C47E/4 turboshaft with dual-channel FADEC; 862 shp takeoff and 761 shp maximum continuous
Crew
1 pilot
Capacity
Standard seating for 1 pilot and 6 passengers; 2,300 lb (1,043 kg) standard internal useful load
Cruise speed
133 kt (246 km/h) maximum cruise
Maximum speed
140 kt (259 km/h) maximum velocity
Range
337 nm (624 km) at long-range cruise; standard maximum gross weight, ISA conditions, standard fuel, sea level and no reserve
Main rotor diameter
35 ft (10.67 m)
Overall length
35 ft (10.67 m)
Maximum takeoff weight
5,000 lb (2,268 kg) standard internal; 5,250 lb (2,381 kg) optional internal; 6,000 lb (2,722 kg) with external load

Related models and variants

References

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