Bell 407

Mid Size Helicopters

ICAO aircraft code B407

Manufacturer Bell Helicopter

Country United States

New price USD 3.1 million (2019)

The Bell 407 is a four-blade, single-engine, civil utility helicopter.

Specifications

Full description

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Bell 407 specifications

General

ICAO aircraft code

B407

Manufacturer

Bell Helicopter

Manufactured

1995 - Present

Country

United States

New purchase price

USD 3.1 million (2019)

Aircraft performance

Avionics:

AP-85 Two-Axis Autopilot, Garmin G1000H/G1000H NXi

Engine:

1x Rolls-Royce Model 250-C47E/4
Turboshaft

Power:

862 HP

Max Cruise Speed:

133 Kts
246 Km/h

Travel range:

337 Nm
624 Kilometers

Fuel Economy:

3.39 Nm / gallon
1.659 Km / liter

Service Ceiling:

20,000 feet

Rate of Climb:

1850 feet / minute
9.40meter / second

Weight & dimensions

Max Take Off Weight:

2,722 Kg
6,001 lbs

Max Payload:

1,156 Kg
2,549 lbs

Fuel Tank Capacity:

128 gallon
484 liter

Baggage Volume:

0.5 m3 / 18 ft3

Disclaimer: The information on this page may not be accurate or current. Never use it for flight planning or any other aircraft operation purposes. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacture or official aviation authorities.

About the Bell 407

The Bell 407 is a four-blade, single-engine, civil utility helicopter. A derivative of the Bell 206L-4 LongRanger, the 407 uses the four-blade, soft-in-plane design rotor with composite hub developed for the United States Army’s OH-58D Kiowa Warrior instead of the two-blade, semi-rigid, teetering rotor of the 206L-4.