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Bell 407GX

Posted on November 10, 2026 By

In March 2011, Bell Helicopter Textron Inc. introduced the multi-purpose single-engine helicopter, the Bell 407GX. By October of the same year, it had received its Federal Aviation Administration (FAA) certification. The first Bell 407GX was delivered to a customer in May of the following year.

Table of Contents

Toggle
    • Key Design and Safety Innovations
    • Performance and Flight Comfort
    • The Bell 407GXP: An Evolution
    • Technical Specifications
  • Image and diagram gallery of the Bell 407GX
    • How to cite this article:

Key Design and Safety Innovations

It differs from the base Bell-407 model with a new instrument panel featuring Garmin G1000H avionics. The helicopter boasts a number of significant safety features, including a digital FADEC system controlling the engine, an artificial terrain display system, a warning system for proximity to other aircraft, a ground collision warning system, and a tail rotor camera.

The sleek, reliable, and impressive Bell 407GX might appear unduly fragile to an inexperienced novice. Its large windows, reduced frames, sweeping fuselage lines, and flexible rotor blades create a deceptive impression of lightness and vulnerability. However, experienced pilots quickly dispel this illusion, understanding that powerful maneuverability potential lies beneath its elegant exterior. In practice, the Bell 407GX quickly proves its capability for passenger and cargo transport, search and rescue, military operations, and as medical transport.

Performance and Flight Comfort

It’s no wonder that sales of Bell 407GX helicopters are popular with both business corporations and major entrepreneurs. While ground travel is most practical by car, the Bell 407GX is an excellent option for quickly covering distances up to 634 km at a cruising speed of 222 km/h. The maximum speed the Bell 407GX helicopter can reach is 246 km/h. For 4.5 hours, 6 passengers choosing charter flights in a Bell 407GX spend their time in comfortable seats, three facing each other, enjoying panoramic views from the huge windows or preferring conversation and multimedia entertainment.

The Bell 407GX’s flight altitude is 6,096 m. Its powerplant features a Rolls-Royce 250-C47B turboshaft engine, capable of handling a full takeoff weight of 2,268 kg, with a useful payload of 1,058 kg. Safety is ensured by innovative Garmin G1000 avionics, which include numerous flight safety monitoring systems, such as dangerous ground proximity, potential mid-air collisions, and detected obstacles. The pilot receives information from two high-resolution LCD displays, showing flight status and digital system data, ensuring helicopter controllability is at the highest level.

Passengers of the Bell 407GX will surely notice the smooth ride and low levels of vibration and noise during flight. As a result, upon completion of the flight, there will be no noise fatigue or discomfort from uncomfortable seats – the Bell 407GX guarantees comfortable travel for every passenger. The passenger cabin is spacious, and the views from the windows will keep boredom at bay during the journey. This stylish and maneuverable Bell 407GX helicopter will make you look at charter flights in a new light. The refined interior, featuring leather, chrome, glass, and wood, transforms a long flight into an unforgettable aerial journey.

The Bell 407GXP: An Evolution

The Bell 407GX stands out for having the lowest price in its class and the best safety, reliability, and other technical parameters. Since 2015, a new modification of the helicopter, the Bell 407GXP, has been released. This helicopter features several differences: a Rolls Royce 250-C47B/8 turboshaft engine with an electronic FADEC control system offers improved performance at high altitudes and in high-temperature conditions. Additionally, the Quiet Cruise™ system significantly reduces in-flight noise levels, and the useful payload has been increased by 53 kg, with an option for an increased maximum takeoff weight.

Technical Specifications

Modification Bell 407GXP
Main rotor diameter, m 10.67
Tail rotor diameter, m 1.65
Length, m 12.62
Height, m 3.29
Width, m 2.29
Empty weight 1244
Normal takeoff weight 2268
Maximum takeoff weight 2722
Internal fuel, l 484 + 72
Engine type 1 Turboshaft Rolls-Royce 250-C47B/8
Power, kW 1 x 643
Maximum speed, km/h 259
Cruising speed, km/h 246
Practical range, km 624
Flight endurance, h 4.0
Rate of climb, m/min 408
Service ceiling, m 5611
Static ceiling, m 3725
Crew 1 crew member
Payload up to 6 passengers or 1160 kg of cargo in cabin or 1200 kg on external sling

Image and diagram gallery of the Bell 407GX

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How to cite this article:

APA: Bell 407GX (). Bell 407GX. wp.archivoaereo.com. https://wp.archivoaereo.com/en/bell-407gx-3/
VANCOUVER: Bell 407GX [online]. wp.archivoaereo.com; [cited 2026-11-11]. Available at: https://wp.archivoaereo.com/en/bell-407gx-3/
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Utility Helicopters Tags:United States

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