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#2398

Bell 407

🇨🇦 Canada ·first flew 1995· multipurpose utility helicopter

🚁 helicopter turboshaft ✓ still flying
Bell 407, photo 1 of 10
1/10 stuart.mike· CC BY 2.0

what is it?

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.

How to recognise it: 1 turboshaft engine · 10.7 m main rotor

base stats

  • speed 259 km/htop speed
  • range 600 kmwithout refuelling
  • size 2,722 kgmax take-off weight
  • built 1,600made in total

Bars compare against all aircraft: 3,500 km/h, 20,000 km, 850 seats; size and number built on a log scale up to 640 t (An-225) and 45,000 built (Cessna 172).

fun facts

  • First flew 31 years ago, in 1995.
  • Top speed is 2.0× a car on the Dutch motorway (130 km/h).
  • Rotor of 10.7 m: about 2 cars parked nose to tail.

turboshaft: A turbine that turns a shaft, usually a helicopter rotor.

spec sheet

first flight
1995-06-29
introduced
1996
status
still flying
number built
1,600
role
multipurpose utility helicopter
origin
🇨🇦 Canada
makers
Bell Textron
engines
1× Allison 250-C47B
length
12.7 m
rotor diameter
10.7 m
height
3.6 m
max take-off weight
2,722 kg
top speed
259 km/h
cruise speed
246 km/h
range
600 km
ceiling
5,697 m

Specs are for the version in the Wikipedia article's specification section. Blank means the sources don't say.

family

Sources: Wikidata Q815682, Wikipedia: Bell 407 (CC BY-SA 4.0).Updated 2026-10-24.

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