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AIR DEFENDER / REFERENCE

Bell 206 JetRanger

Single-turbine light helicopter · Bell 206B JetRanger II

Aircraft overview

The Bell 206B JetRanger is a light, single-turbine helicopter with a two-bladed main rotor, a two-bladed tail rotor and skid landing gear. The cabin provides a pilot’s position and up to four passenger places.

The JetRanger II uses a Rolls-Royce/Allison 250-C20 engine, with different installed power and loading limits from later JetRanger and LongRanger configurations.

White, blue and gold Bell 206B G-OPEN hovering, with the complete visible main rotor, cabin, tail and skids inside the frame.
Bell 206B-3 G-OPEN, photographed on 13 June 2010. The specification below describes the early JetRanger II with the 250-C20 engine.
Photograph: Tony Hisgett · 2010-06-13 · Photo source: G-OPEN Bell Helicopters 206B-3 (4701333138) · CC BY 2.0 · Unmodified photograph.

At a glance

Bell 206B JetRanger II · early 250-C20 configuration

Engine
One 250-C20 turboshaftRolls-Royce/Allison 250-C20 installation.
Installed continuous / take-off power
270 /317 hpTake-off rating limited to five minutes.
Main rotor
Two blades ·10.16 m diameterSeparate from overall rotor-running length.
Tail rotor
Two blades ·1.65 m diameterConventional tail rotor.
Fuselage length
9.50 mBody length; does not include the full rotor-running envelope.
Maximum normal internal weight
3,200 lb ·1,451 kgBaseline reference; optional or external-load configurations have separate conditions.
Cabin
One pilot + up to four passengersMaximum passenger arrangement; actual interiors differ.

In Air Defender

Role guidance · v0.8.16.0

Air Defender v0.8.16.0 includes the Bell 206 JetRanger as a civilian-helicopter reference. The catalogue description does not establish the load or purpose of an individual contact.

Compare the larger Bell 407, then use Aircraft Data and flight-plan information for the selected flight.

Game catalogue values · v0.8.16.0

In-game specifications

These figures come from the game’s general aircraft reference. A matching civilian register entry can supply different fields in Aircraft Data. How to read the two layouts →

Role
Light Utility Helicopter
Category
Light Helicopter
Service ceiling
13,500 ftA reference upper height. Read Flight Info for the contact’s present height.
Maximum speed
120 knotsA reference maximum, not the speed the aircraft is flying now.
Cruise speed
110 knotsA typical speed for the main part of a flight, not a guaranteed commanded speed.
Stall speed
Not specified as a stall-speed valueA zero in the game catalogue means no usable stall-speed figure is supplied; it does not mean the rotor blades cannot stall. FAA helicopter handbook: rotor-blade stall →
Typical range
370 NMA reference flying distance, not fuel remaining or radar detection range.
Typical crew
1
Powerplant
Single turboshaft engine (Allison 250) Compare engine types →
Manufacturer
Bell Helicopter (USA)
Understand speed, ceiling, range and the units →

Use the right procedure

In depth

Rotor and airframe layout

The 206B uses two blades in both its main and tail rotors. The main rotor is 10.16 m across, and the tail rotor is 1.65 m across.

The published body dimensions describe the fuselage and skids. They are not the total space occupied by the rotor tips while running.

Installed turbine power

The JetRanger II uses the 250-C20 turboshaft. Its installed limits are 317 hp for five minutes and 270 hp continuously.

Those power limits apply to the JetRanger II’s 250-C20 installation. A rating for another 250-series engine does not give the permitted power for this helicopter.

Cabin and loading

The 206B accommodates one pilot and up to four passengers. Its normal gross-weight limit is 3,200 lb (1,451 kg).

External-load approvals have separate conditions and do not create an equivalent increase in cabin loading. Seats, fuel, baggage and installed equipment remain part of the relevant weight calculation.

Fuel and configuration

The early 206B fuel installation provides 288 litres of usable fuel. A 344-litre arrangement applies from serial 3567; the later capacity is separate from the early JetRanger II configuration.

Reference tank capacity describes an installation, not the amount remaining during a flight. The aircraft’s weight and centre-of-gravity limits continue to govern its loaded condition.

Type and configuration development

The 206B received its original FAA approval on 19 August 1971. The early serial groups identified as JetRanger II are distinct from later 206B configurations covered elsewhere in the type certificate.

Variants

206B JetRanger II

Early 250-C20 configuration, with serial applicability specified in the type record.

Later 206B configurations

Different approved engines and serial groups; their limits are separate.

References and further reading

Named configuration, rotors, installed power, cabin, loading and model history

Words used on this page

Choose an underlined term for a quick explanation, or browse the meanings here.

Landing gear

The wheels, skids or floats and their supporting structure used when an aircraft lands. Fixed gear stays outside the aircraft; retractable gear can fold away. A tricycle layout has nose gear at the front and main gear behind it.

How to read aircraft specifications
Turboshaft

A gas-turbine engine supplying shaft power to equipment such as helicopter rotors, rather than relying mainly on exhaust thrust.

Related guide: aircraft engines
Contact

Something detected or being followed on the display. You may still need to establish what it is.

Related guide: plot or track
Flight plan

Information about an intended flight, such as its route and destination. Compare that plan with what the aircraft is actually doing.

Related guide: flight plans
Service ceiling

The stated height an aircraft can climb to while still meeting specified performance requirements. The game’s reference figure is not its current height or a guarantee for every situation.

How to read aircraft specifications
Feet / ft

A unit of length used here for aircraft height. Read the display’s scale: a trackblock height of 350 means 35,000 feet, not 350 feet.

Related guide: trackblock
Knots

A unit of speed used in aviation: nautical miles per hour.

Related guide: trackblock
Cruise speed

A speed used for the main travelling part of a flight. A reference cruise speed is different from a track’s current speed.

Related guide: interceptor speed
Stall speed

A reference speed for the onset of a stall under specified conditions. A stall occurs when a wing or rotor blade exceeds its critical angle to the airflow and loses lift. It does not mean the engine has stopped.

How to read aircraft specifications
FAA

Federal Aviation Administration: the United States aviation authority.

How to read aircraft specifications
Range

Distance. For a contact it means distance from a stated point; an aircraft’s range means how far it can fly under stated conditions.

Related guide: range bearing
Nautical mile / NM

A distance unit used in aviation and navigation. It is different from the ordinary mile used on UK road signs.

Related guide: range bearing
Powerplant

The engine or engines that power the aircraft.

How to read aircraft specifications
Type certificate

Official approval of an aircraft design against the rules that apply to that design. It does not describe the condition of one aircraft on today’s flight.

How to read aircraft specifications
IN PLAIN ENGLISH

Read the guide →