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AIR DEFENDER / REFERENCE

De Havilland Canada DHC-6 Twin Otter

Utility turboprop · DHC-6 Series 100

Aircraft overview

The DHC-6 Twin Otter is a twin-turboprop utility and commuter aircraft developed from the single-engined DHC-3 Otter. It first flew in 1965. The original Series 100 has a short nose, PT6A-20 engines and an unpressurised cabin for up to 19 passengers.

The family developed through changes to nose length, baggage space and engine power. The specifications below describe the original short-nose Series 100 landplane. The Series 200, 300 and modern 400 have different configurations.

DHC-6 Twin Otter SX-BVP on floats, with a high wing and two propellers; a ground trolley sits beneath it.
DHC-6 Series 300 Twin Otter SX-BVP on floats, photographed in 2009. The specification below describes the earlier Series 100 landplane.
Photograph: Kecko · 19 July 2009 · Photo source: De Havilland Canada DHC-6-300 Twin Otter @ Airport St.Gallen-Altenrhein · CC BY 2.0 · Proportionally resized; no crop.

At a glance

DHC-6 Series 100 · short-nose landplane, serials 6–115, without weight-increase Mod 6/1020; specification dated November 2011

Engines
Two Pratt & Whitney Canada PT6A-20 turbopropsOriginal Series 100.
Passenger seats
Up to 19Series 100; crew separate.
Minimum crew in the type certificate
One pilotOperating requirements may call for more crew.
Baseline take-off / landing mass
11,000 lb / 11,000 lbWheeled landplane without Mod 6/1020.
Nominal propeller diameter
8 ft 6 inHartzell installation; a smaller repair minimum is separately permitted.
Standard usable fuel
1,432 litres686 litres forward + 746 litres rear; optional tanks excluded.
Baggage compartment limits
Front 91 kg / rear 227 kgOriginal short-nose arrangement; individual compartment limits.

In Air Defender

Role guidance · v0.8.16.0

Air Defender v0.8.16.0 includes the general DHC-6 Twin Otter as a utility transport. Its catalogue crew figure is separate from the real Series 100’s certificate minimum; the general game label does not specify a series or landing-gear fit.

Compare the pressurised Beechcraft 1900 and use Aircraft Data and flight plans to investigate the contact. Short-field capability does not establish a new player command or an unrestricted landing location.

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
Utility Transport
Category
Regional Aircraft
Service ceiling
25,000 ftA reference upper height. Read Flight Info for the contact’s present height.
Maximum speed
182 knotsA reference maximum, not the speed the aircraft is flying now.
Cruise speed
160 knotsA typical speed for the main part of a flight, not a guaranteed commanded speed.
Stall speed
51 knotsA reference for specified conditions. Stalling means the wing loses lift, not that an engine stops.
Typical range
806 NMA reference flying distance, not fuel remaining or radar detection range.
Typical crew
2
Powerplant
Twin turboprop engines (Pratt & Whitney Canada PT6A) Compare engine types →
Manufacturer
De Havilland Canada (Canada)
Understand speed, ceiling, range and the units →

Use the right procedure

In depth

From Otter to Twin Otter

The DHC-6 developed the single-piston-engined Otter into a twin-turboprop aircraft. The Series 100 was the original short-nose production version. The Series 200 lengthened the nose and increased rear baggage space; the Series 300 introduced more powerful PT6A-27 engines and a 12,500 lb maximum authorised weight.

PT6A-20 engines and propellers

The Series 100 has two PT6A-20 engines driving Hartzell propellers. Turbine power turns the propeller, which produces the main thrust. The nominal diameter is 8 ft 6 in; the certificate separately permits a minimum diameter after repairs.

Cabin and baggage compartments

The unpressurised commuter cabin has up to 19 passenger seats. The original short-nose front baggage compartment is limited to 91 kg, while the rear compartment is limited to 227 kg. These are separate compartment limits, not a complete aircraft payload allowance.

Standard fuel tanks

The forward tank holds 686 litres of usable fuel and the rear tank 746 litres, giving a standard total of 1,432 litres. Unusable fuel is accounted for separately; it is not an additional reserve available to the pilot.

Landplane, ski and float configurations

The unmodified Series 100 landplane uses the earlier Series 1’s 11,000 lb take-off and landing limits. Weight-increase modification 6/1020 introduces different limits and temperature conditions; ski and float installations also have their own provisions.

A long-nose modification can change the aircraft’s configuration. A generic Twin Otter dimension or baggage figure therefore needs its series and nose arrangement attached.

Variants

Series 100

Original production version with a short nose and PT6A-20 engines.

Series 200

Longer nose and increased rear baggage capacity.

Series 300

More powerful PT6A-27 engines and a 12,500 lb maximum authorised weight.

Series 400

Modern generation with updated avionics and flexible mission interiors, separate from the original Series 100.

After 1998

Series 400

The Series 400 has Honeywell Apex avionics and configurable interiors for passenger, cargo, medical and special-mission work. These later features are separate from the original Series 100 configuration.

References and further reading

Original development, cabin and early variants

Series 100 engines, fuel, loading and baseline limits

Modern Series 400 context

Turboprop principle

Words used on this page

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

Turboprop

A gas-turbine engine driving a propeller through a shaft and gearbox. The propeller supplies most of its thrust.

Related guide: aircraft engines
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
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
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
Contact

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

Related guide: plot or track
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
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
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
Payload

What the aircraft carries for the job. In a supply order, this means the cargo you choose to deliver.

Related guide: supply cargo
IN PLAIN ENGLISH

Read the guide →