De Havilland Canada DHC-3 Otter

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The de Havilland Canada DHC-3 Otter is a single-engined, high-wing, propeller-driven, short take-off and landing (STOL) aircraft developed by de Havilland Canada. It was conceived to be capable of performing the same roles as the earlier and highly successful Beaver, including as a bush plane, while also being a larger aircraft. The type certificate of the aircraft is now owned by the De Havilland Canada founded in 2019.

Design and development

The rugged single-engined, high-wing, propeller-driven DHC-3 Otter was conceived in January 1951 by de Havilland Canada as a larger, more powerful version of its highly successful DHC2 Beaver STOL utility transport. Dubbed the "King Beaver" during design, it would be the veritable "one-ton truck" to the Beaver's "half-ton" role.<ref>Rossiter 1998, p. 55.</ref>

The Otter received Canadian certification in November 1952 and entered production shortly thereafter. Using the same overall configuration as the Beaver, the new, much heavier design incorporated a longer fuselage, greater-span wing, and cruciform tail. Seating in the main cabin expanded from six to 10 or 11. Power was supplied by a 450-kW (600 hp) Pratt & Whitney R-1340 geared radial. The version used in the Otter was geared for lower propeller revolutions and consequently lower airspeed. The electrical system was 28 volts D.C.

Like the Beaver, the Otter can be fitted with skis or floats. The Otter served as the basis for the very successful Twin Otter, which features two wing-mounted Pratt & Whitney Canada PT6 turboprops. A total of 466 Otters were manufactured.<ref>Template:Cite news</ref>

Operational use

U.S. Army U-1A, July 1967 Hue Citadel Airfield, Republic of Vietnam
Otter on floats, powered by a PZL Kalisz ASz-62IR with four blade propeller
F/L Lynn Garrison and crew with UNEF Otter, Sinai, 1962
Turbo Otter on wheel-skis
U.S. Navy U-1B (UC-1) Otter at NAS Pensacola, Florida, in 2002
Otter with turbine engine conversion, covered against the cold on Mistassini lake, Mistissini, Quebec

The DHC-3/CC-123/CSR-123 Otter was used until 1980 by the Royal Canadian Air Force and its successor, the Air Command of the Canadian Forces. It was used in Search and Rescue, as the "CSR" denotes Canadian Search (and) Rescue (type 123) and as a light utility transport, "CC" denoting Canadian Cargo. During the Suez Crisis, the Canadian government decided to provide assistance to the United Nations Emergency Force and the Royal Canadian Navy carrier Template:HMCS carried 4 Otters from Halifax to Port Said in Egypt early in 1957, with all four flying off unassisted while the ship was at anchor.<ref name=Maggie>Template:Cite news</ref> This was the only occasion when RCAF fixed wing aircraft operated from a Canadian warship.<ref name=Maggie /> It was also operated on EDO floats on water and skis for winter operations on snow. The EDO floats also had wheels for use on runways (amphibious). It was used as army support dropping supplies by parachute, and also non-parachute low-speed, low-altitude air drops, to support the Canadian Army on manoeuvres. In the end it was operated by the Primary Air Reserve in Montreal, Toronto, Edmonton and Winnipeg, with approximately 10 aircraft at each base, as well as by the RSU (Regular (Forces) Support Units) at those bases. It was usually flown with a single pilot (Commissioned Officer) in the left seat and a Technical Air Crewman (NCO) in the right seat. The Kiowa helicopter replaced it in Air Reserve squadrons.

Although the Otter found ready acceptance in bush airlines, as in a similar scenario to the DHC-2 Beaver, the United States Army soon became the largest operator of the aircraft (184 delivered as the U-1A Otter). Other military users included Australia, Canada, and India, but the primary role of the aircraft as a rugged bush plane continues to this day.

An Otter crossed the South Pole in 1957 (see Commonwealth Trans-Antarctic Expedition). The Otter is also popular in the skydiving community and can be found in many drop zones throughout the world.

Otters were used by Qantas from 1958 to 1960 in Papua New Guinea. The Qantas aircraft were then transferred to Trans Australian Airlines (TAA), a major Australian domestic airline, which operated the Otters in Papua New Guinea until 1966 when they were withdrawn from use. TAA was merged with Qantas in 1990.

Modifications

The most extensively modified Otter was RCAF Otter 3682. After initial service as a standard Search and Rescue aircraft it was used to explore the aerodynamic aspects of STOL. In 1958, it was fitted with flaps so outsized that, with their 45 degree droop, it became known as the Batwing Otter. In addition, its tail-wheel undercarriage was replaced with a high energy-absorption 4-wheel arrangement and a very high vertical tail. The next modification replaced the flaps with fully retractable flaps suitable for cruising flight and high drag was obtained with reverse thrust from a J85 turbojet installed in the fuselage behind the cockpit. The third configuration looked a lot like the future Twin Otter and was the first twin-PT6 fixed-wing installation to fly in May 1963 (A twin PT6-engined helicopter, the Kaman K-1125, had flown in April 1963). The piston engine in the nose was replaced with wing-mounted engines to blow over the flaps.<ref>https://www.flightglobal.com/pdfarchive/view/1963/1963%20-%200073.html?search=january%20stol%20otter Template:Dead link</ref><ref>Power – The Pratt & Whitney Canada Story, Kenneth H. Sullivan and Larry Milberry, CANAV Books 1989, Template:ISBN, p. 147</ref><ref>The Universal Airplanes – Otter & Twin Otter, Sean Rossiter 1998, Douglas & McIntyre, Template:ISBN, pp. 13–31</ref>

Stolairus Aviation of Kelowna, BC, has developed several modifications for the DHC-3 including a STOL Kit, which modifies the wing with a contoured leading edge and drooped wingtips for increased performance. Stolairus has also developed a Template:Convert "upgross" kit which increases the gross weight of the DHC-3 to Template:Convert on floats.<ref>"DHC-3 Otter." Stolairus, Retrieved: 2 February 2012.</ref>

Some aircraft were converted to turbine power using a PT6A, Walter 601 (manufactured in the Czech Republic), or Garrett/Honeywell TPE331-10, by Texas Turbine Conversions. The Walter M601E-11 Turbine Engine conversion is manufactured and installed by Stolairus Aviation.

A Polish PZL radial engine has also been fitted. Re-engined aircraft have been offered since the 1980s by Airtech Canada as the DHC-3/1000 using current-production 1,000 hp (745 kW) PZL ASz-62 IR radials.<ref name="Janes 88 p17">Taylor 1988 p. 17.</ref>

Variants

DHC-3 Otter
Single-engined STOL utility transport aircraft.
CSR-123 Otter
STOL utility transport aircraft for the Royal Canadian Air Force.
YU-1 Otter
Six test and evaluation aircraft for the U.S. Army.
U-1A Otter
STOL utility transport aircraft for the U.S. Army.
UC-1 Otter
STOL utility transport aircraft for the United States Navy. Later redesignated U-1B Otter in 1962.
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Otters fitted with either Pratt & Whitney Canada PT6A-27 or Pratt & Whitney Canada PT6A-34 turboprop engine.
Airtech Canada DHC-3/1000 Otter
Conversions powered by PZL Kalisz ASz-62IR engines.<ref name="Janes 88 p17"/>
Texas Turbines Super Otter
Turbine conversion powered by a Template:Cvt Garret TPE331 turboprop engine
Aerotech Industries
Turbine conversion powered by a 900shp Pratt & Whitney Canada PT6A-140A turboprop engine.[1]

Military operators

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  • Royal Australian Air Force: Two Otters (RAAF serial A100-1 and 2) were in service with the RAAF from 1961 to 1967. The aircraft were used for passenger and freight transport duties at the Weapons Research Establishment, Woomera, South Australia.
    • No. 1 Air Trials Unit
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  • Ghana Air Force – acquired twelve Otters (G300 – G311), in service 1961-1973 (serial number: 413, 414, 416, 418, 420, 422, 424, 425, 426, 428, 430, 431).<ref>{{#invoke:citation/CS1|citation

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    • Four aircraft had to be written off, eight aircraft were sold in 1973.
      • G300 (s/n 413) crashed on 21 June 1968 in the jungle in the Brong Ahafo region of Ghana and was destroyed.
      • G301 (s/n 414) crashed on 31 August 1961 at Kintampo in the Brong Ahafo region of Ghana and was destroyed.
      • G302 (s/n 416) crashed on the beach near Takoradi on a date unknown and was destroyed. It was on floats at the time, on a training detail.
      • G308 (s/n 426) was written off in service.
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Civil operators

DHC-3-T Turbo Otter on Lake Union, Seattle, WA
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Accidents

As of June 2019, there have been 119 incidents and accidents involving the DHC-3 resulting in 242 deaths.<ref>{{#invoke:citation/CS1|citation |CitationClass=web }}</ref> Listed below are a select few of the most notable ones.

  • In 1956, two military Otters broke up in mid-air. One had taken off from Downsview and the other from Goose Bay. The Otter requires immediate use of elevator trim to counteract the strong change in pitch caused by the retraction or extension of the flaps. Investigators found that metal contamination in a hydraulic valve allowed the flaps to rapidly retract with the tailplane still fully trimmed, and the consequent nose drop was severe enough to cause structural failure. A filter was added to the flap hydraulic system and an interconnection added between the flaps and tailplane to maintain proper trim as the flaps are operated.<ref>Air Crash – The Clues in the Wreckage, Fred Jones 1985, Roobert Hale Ltd., Template:ISBN, pp. 104–112</ref>
  • On 20 May 1964, Philippines Airlines Flight F26, a DHC-3 Otter, PI-C51, crashed into a hill when flying at VFR at Subico Point, killing all 11 on board.
  • On 24 March 1986, a DHC-3 Otter floatplane, C-FAGM, of Labrador Airways, crashed while returning to Goose Bay Airport from a trip to Snegamook Lake to retrieve a group of partridge hunters. On the return trip, the aircraft encountered engine trouble. The pilot, Howard Mercer, who was the president of Goose Bay Air Services, called dispatch to report the engine running rough. As the aircraft neared Nipishish Lake, 47 miles north of Goose Bay, the pilot reported experiencing engine problems again, and that he would follow the Crooked River towards the airport as a precautionary measure for if an emergency landing was needed. Three minutes later, the pilot called dispatch to inform them he would be making an emergency landing on the river due to a smoke odour in the cockpit. The aircraft never made it. Due to whiteout conditions and the frozen surface of the river, when the pilot flew close to the ground to land, the wing struck the ground and the aircraft broke apart and was subsequently engulfed in flames. Three passengers and the pilot were killed, while one passenger survived the crash with serious injuries.<ref>{{#invoke:citation/CS1|citation

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  • On 15 September 2015, a DHC-3 Turbine Otter floatplane carrying ten people and belonging to Rainbow King Lodge crashed on takeoff at Eastwind Lake, Template:Cvt mile north of Iliamna, Template:Cvt southwest of Anchorage. Three people were killed in the crash.<ref>Template:Cite news</ref>
  • On 13 May 2019, in the 2019 Alaska mid-air collision, a Taquan Air DHC-3 Turbine Otter floatplane, N959PA, collided with a Mountain Air Service DHC-2 Beaver, N952DB, over George Inlet, Alaska, with the loss of one passenger aboard the DHC-3 and five passengers and crew aboard the DHC-2. The NTSB attributed the accident to Template:" 'the inherent limitations of the see-and-avoid concept, along with the absence of alerts from both airplanes' traffic display systems." Due to the angle of approach, both pilots' viewpoints were partially blocked by the aircraft structure or seated passengers. The NTSB identified Taquan's inadequate preflight checklist and the Federal Aviation Administration's failure to require Taquan to implement a safety management system as contributing factors.<ref>Template:Cite report</ref>
  • On 4 September 2022, a DHC-3 floatplane operated by Friday Harbor Seaplanes, N725TH, crashed in Puget Sound near Whidbey Island, Washington, killing all ten aboard the aircraft.<ref>{{#invoke:citation/CS1|citation

|CitationClass=web }}</ref> On October 24, the NTSB announced that the horizontal stabilizer actuator had separated into two pieces at a threaded assembly fitting, and that the actuator lock ring was missing from the wreckage.<ref>{{#invoke:citation/CS1|citation |CitationClass=web }}</ref><ref name="DCA22MA193 investigative update">{{#invoke:citation/CS1|citation |CitationClass=web }}</ref> The next day, Viking Air issued a service letter requiring DHC-3 Otter operators to inspect their aircraft and ensure that the actuator's lock ring is present.<ref name="service letter">{{#invoke:citation/CS1|citation |CitationClass=web }}</ref>

Specifications (landplane)

3-view line drawing of the de Havilland Canada U-1A Otter
3-view line drawing of the de Havilland Canada U-1A Otter

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See also

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References

Notes

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Bibliography

  • Hayes, Karl E. DHC-3 Otter – A History (CD-ROM). Crakaig, Killiney Hill Road, Killiney, Co. Dublin, Ireland: Karl E. Hayes Publisher, 2006. (also available via CANAV Books, Toronto)
  • Hotson, Fred W. The de Havilland Canada Story. Toronto: CANAV Books, 1983. Template:ISBN.
  • Michell, Simon. (ed.). Jane's Civil and Military Aircraft Upgrades 1994–95. Coulsdon, UK: Jane's Information Group, 1994. Template:ISBN.
  • Milberry, Larry. Aviation in Canada. Toronto: McGraw-Hill Ryerson Ltd., 1979. Template:ISBN.
  • Molson, Ken M. and Harold A. Taylor. Canadian Aircraft Since 1909. Stittsville, Ontario: Canada's Wings, Inc., 1982. Template:ISBN.
  • Template:Cite journal
  • Rossiter, Sean. The Immortal Beaver: The World's Greatest Bush Plane. Vancouver: Douglas & McIntyre, 1999. Template:ISBN.
  • Rossiter, Sean. Otter & Twin Otter: The Universal Airplanes. Vancouver: Douglas & McIntyre, 1998. Template:ISBN.
  • Template:Cite journal
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  • Taylor, John W.R., ed. Jane's All The World's Aircraft 1988–89. Coulsdon, UK: Jane's Defence Data, 1988. Template:ISBN.

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