De Havilland Canada
DHC-6
Twin Otter

Photo: Robert Deering 4/21/2025
Burrard Inlet
Vnacouver, BC, Canada

The de Havilland Canada DHC-6 Twin Otter is a Canadian STOL (Short Takeoff and Landing) utility aircraft developed by de Havilland Canada in the mid-1960s and still in production today. Built by De Havilland Canada from 1965 to 1988, Viking Air purchased the type certificate and restarted production in 2008, before re-adopting the DHC name in 2022. In 2023 DHC restarted production of the 300 series, in addition to the Series 400 produced by Viking.

The aircraft's fixed tricycle undercarriage, STOL capabilities, twin turboprop engines and high rate of climb have made it a successful commuter airliner, typically seating 18–20 passengers, as well as a cargo and medical evacuation aircraft. In addition, the Twin Otter has been popular with commercial skydiving operations, and is used by the United States Army Parachute Team and the 98th Flying Training Squadron of the United States Air Force.

VARIANTS

Civilian Aircraft
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DHC-6 Series 100: Twin-engine STOL utility transport aircraft, powered by two 550 shp (410 kW) Pratt & Whitney PT6A-20 turboprop engines.
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DHC-6 Series 110: Variant of the Series 100 built to conform to BCAR (British Civil Air Regulations).
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DHC-6 Series 200: Improved version.
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DHC-6 Series 300: Twin-engine STOL utility transport aircraft, powered by two 680 shp (510 kW) (715 ESHP) Pratt & Whitney Canada PT6A-27 turboprop engines.
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DHC-6 Series 300M: Multi-role military transport aircraft. Two of these were produced as "proof-of-concept" demonstrators. Both have since been reverted to Series 300 conformity.
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DHC-6 Series 310: Variant of the Series 300 built to conform to BCAR (British Civil Air Regulations).
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DHC-6 Series 320: Variant of the Series 300 built to conform to Australian Civil Air Regulations.
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DHC-6 Series 300S: Six demonstrator aircraft fitted with eleven seats, wing spoilers and an anti-skid braking system. All have since been reverted to Series 300 conformity.
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Viking Air DHC-6 Series 400: Viking Air production, first delivered in July 2010, powered by two Pratt & Whitney Canada PT6A-34 engines, and available on standard landing gear, straight floats, amphibious floats, skis, wheel skis, or intermediate flotation landing gear ("tundra tires").
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Viking Air DHC-6 Series 400S Seaplane - never produced: Viking Air seventeen-seat seaplane version of the Series 400 with twin floats and corrosion-resistance measures for the airframe, engines and fuels system. Customer deliveries planned from early 2017. 500 lb (230 kg) lighter than the 400.
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DHC-6 Classic 300-G: Updated DHC-6 Series 400, with an all-new interior and new flight deck featuring a glass cockpit.
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Military Aircraft
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CC-138: Twin-engine STOL utility transport, search and rescue aircraft for the Canadian Armed Forces Search and Rescue operations. Based on the Series 300 aircraft.
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UV-18A: Twin-engine STOL utility transport aircraft for the Alaska National Guard. Six built. It has been replaced by the Short C-23 Sherpa in United States Army service. In 2019 the United States Naval Research Laboratory added a UV-18A to the Scientific Development Squadron One (VXS-1) inventory.
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UV-18B: Parachute training aircraft for the United States Air Force Academy. The United States Air Force Academy's 98th Flying Training Squadron maintains three. UV-18s in its inventory as free-fall parachuting training aircraft, and by the Academy Parachute Team, the Wings of Blue, for year-round parachuting operations. Based on the Series 300 aircraft.
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UV-18C: United States Army designation for three Viking Air Series 400s delivered in 2013.
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SPECIFICATIONS (300): PERFORMANCE:
Span:  65 ft 0 in (19.81 m) Maximum cruise:  338 km/h (182 kn)
Length:  51 ft 9 in (15.77 m) Range:  945 mi (822 nmi, 1,520 km)
Height:  19 ft 6 in (5.94 m) Service ceiling:  25,000 ft (7,620 m)
Empty Weight:   7,415 lb (3,363 kg)  
Gross Weight:  12,500 lb (5.670 kg)  
Crew: 1-2 and up to 20 passengers
Engines:  2 × Pratt & Whitney PTA6A-27 engines, 620 shp (460 kW)
   
SOURCE:  Wikipedia