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Bell 407GXP

Bell 407GXP

Civil Helicopters
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Basic Information
Name
Bell 407GXP
Designation
Bell 407GXP
Alternate Designation
Bell 407GXi
Equipment Type
Civil Helicopters
Manufacturer
Bell Textron
Date of Introduction
2016
Description

The Bell 407GXP is a light, single-engine, commercial helicopter derived from the Bell 407GX offering performance improvements, payload increase (50-pound) and pilot workload reduction. The helicopter is powered by a single engine Rolls-Royce M250-C47B featuring Full Authority Digital Electronic Control (FADEC). The aircraft is also equipped with new avionics features such as a hover performance calculator improvement, as well as a transmission TBO extension of +500 hours that will lower maintenance costs. The Bell 407GXP suits corporate, Emergency Medical Service (EMS), homeland security and utility helicopter roles. Bell Helicopter launched this aircraft at Heli-Expo on March 3, 2015. Deliveries are slated to start before the end of 2015.

Air & Air Defense Specifications
Crew 2
Max Speed 252.0 km/h
Range 612.0 km
Service Ceiling 6096 m
Overview (Deagel)
Group Civil Helicopters
Status Active
Also Known As Bell 407GXi
Origin United States of America
Contractor Bell Textron
Initial Operational Capability (IOC) January 18, 2016
First Flight February 2015
Total Production 409
Specifications (Deagel)
Crew 2
Main Rotor Blades 4
Number of Engines 1
Passengers 5
Dimensions — Height 3.3 meter
Dimensions — Length 10.6 meter
Dimensions — Main Rotor Diameter 10.7 meter
Dimensions — Width 2.5 meter
Mass — Max Takeoff Weight 2,722 kilogram
Performance — Ceiling 6,096 meter
Performance — Max Range 612 kilometer
Power — Max Power at TakeOff 701 shp
Speed — Cruise Speed 219 kph
Speed — Top Speed at High Altitude 252 kph
Time — Flight Endurance 4.5 hour
Gear (Deagel)
Item 1 Turboprop Engines: M250-C47B (1)
Variants
Variant 1 Bell 427
Variant 2 OH-58F Kiowa Warrior
Variant 3 OH-58D Kiowa Warrior
Variant 4 Bell 407
Variant 5 ARH-70A
Variant 6 Bell 407GT
Variant 7 Bell 407GXP
Details
Country of Origin United States
Category Rotary Wing Aircraft
Air > Rotary Wing Aircraft
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
10.6 m
Width
2.5 m
Height
3.3 m
Weight
2722 kg
Operators (18)
China
United States
Germany
United Kingdom
Japan
Ukraine
Poland
India
Brazil
South Africa
Argentina
Canada
Ireland
Mexico
Nepal
Nigeria
Panama
Taiwan
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