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DHC-6 Twin Otter

Classic 300-G

Taking an iconic aircraft to new heights

Taking an iconic aircraft to new heights

For over 50 years, the DHC-6 Twin Otter has stood alone as the most reliable and versatile aircraft in its class. After extensive consultation with customers, De Havilland Canada is poised and proud to take this iconic aircraft to new heights with the new DHC-6 Twin Otter Classic 300-G™.

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The Small Utility Aircraft of Choice

Short Take-Off & Landing Capability (STOL)
1,200 ft (366 m) take-off and 1,050 ft (320 m) landing field length
Variety of Landing Gear Configurations
Wheels, Floats, Amphibious Floats, Wheel Skis, Skis, Intermediate Flotation Gear
Flexible Interior Configurations
All Passenger, All Cargo, Quick Change, Dual-Class, VIP, Paratroop, Special Mission
Dual or Single Pilot Operation

Made Better

More Payload, More Range
New Flight Deck
Two Engine Options
Redesigned Cabin Interior
Lower Operating Costs and Enhanced Dispatch Availability
De Havilland Canada DHC-6 Twin Otter 300-G wheels right side view
De Havilland Canada DHC-6 Twin Otter 300-G cabin upgrades
De Havilland Canada DHC-6 Twin Otter 300-G wheels configuration side cut-away view to show interior
De Havilland Canada DHC-6 Twin Otter 300-G cabin upgrades from above
De Havilland Canada DHC-6 Twin Otter 300-G amphibious floats right side view
De Havilland Canada DHC-6 Twin Otter 300-G amphibious floats close-up of cargo and passenger doors open

Garmin G1000® NXi Flight Deck

  • Fully integrated avionics suite with functionality and capability to meet current and future ATC requirements
  • Autopilot, FMS, Weather Radar, Satellite Communications, Ground Proximity Warning, Traffic Advisory, Flight Tracking System, Synthetic Vision, Video Display, and more

A Completely Redesigned Cabin Interior

  • Modern design blending aesthetics and functionality
  • Redesigned window reveal providing more natural light and brighter cabin ambiance
  • New integrated Passenger Service Units featuring LED lights and gaspers for improved passenger comfort and convenience

Two Engine Options — Economy Meets Performance

  • Standard PT6A-27 engine is the economical choice, providing efficient performance and fuel consumption
  • Optional PT6A-34 engine is designed for extreme operations, ideal for challenging environments and demanding missions
  • New starter generators with cross generator start paired with a lithium chemistry battery offer powerful and reliable starting capabilities

More Payload, More Range

  • 400–500 lb basic weight reduction
  • Weight reduction gives more payload and/or longer range capability
  • Overall, 8% increase in revenue

Lower Operating Costs and Enhanced Dispatch Availability

  • More robust systems with longer service life and extended time between overhauls
  • New cabin interior utilizing new and durable materials with reduced part count
  • Zonal Maintenance Program consolidates inspections/checks, and eliminates duplication and re-inspection
  • Less time on the ground for maintenance means more flying time

Exterior

Specifications

(Standard Wheel Configuration)

Design Weight

Maximum Take-Off Weight 5,670 kg 12,500 lb
Maximum Landing Weight 5,579 kg 12,300 lb

Short Take-Off and Landing Performance*

Take-Off Distance to 50 ft (15.2 m) 366 m 1,200 ft
Landing Distance from 50 ft (15.2 m) 320 m 1,050 ft

SFAR 23 Take-Off and Landing Distance

Take-Off Distance to 50 ft (15.2 m) 454 m 1,490 ft
Landing Distance from 50 ft (15.2 m) 460 m 1,510 ft
Accelerate-Stop Distance 675 m 2,220 ft

Speed

Maximum Cruise Speed - Sea Level 170 KTAS
Maximum Cruise Speed - 5,000 ft 181 KTAS
Maximum Cruise Speed - 10,000 ft 182 KTAS

Payload and Range Capability

Payload for 100 nm (185 km) Range 1,963 kg 4,328 lb
Payload for 250 nm (463 km) Range 1,754 kg 3,868 lb
Maximum Range (Zero Payload) 1,613 km 871 nm
Maximum Range (2,270 lb (1,030 kg) of Payload) 1,487 km 803 nm

Dimensions

This website and/or the information contained herein may not be reproduced in whole or in part without DHC’s prior written consent. Website material is submitted for informational purposes only, is not part of any proposal and creates no contractual commitment. DHC provides the information contained on this website on an ‘as is, where is’ basis and makes no representation or warranty of any kind regarding the applicability or reliability of any of such information with respect to any use whatsoever to be made of it by the recipient. Any information of a technical nature on this website may contain inaccuracies and is subject to change and should never be relied upon for operational use.

*Local regulatory approval required

**Standard fuel tanks; Payload estimates based on Maximum Cruise Rating speed @ 10,000 ft; Maximum Range estimates based on Long Range Cruise speed @ 10,000 ft; 45-minute reserve fuel @ cruise altitude and Maximum Endurance Speed

For more information about aircraft flexibility and customization, contact sales@dehavilland.com.