Canadair CL-44

Canadair Out of production since 1965
1959First flight
39Units built
160Typical passengers
4,627 kmRange
3On Vuelopedia
Canadair CL-44 illustration Illustrative image; it may differ from the actual aircraft.

The Canadair CL-44 was a Canadian turboprop airliner and cargo aircraft based on the Bristol Britannia that was developed and produced by Canadair in the late 1950s and early 1960s. Although innovative, only a small number of the aircraft were produced for the Royal Canadian Air Force (RCAF) (as the CC-106 Yukon), and for commercial operators worldwide. The aircraft is named after the Canadian territory of Yukon.

Specifications

Figures for the CL-44D4 variant, the most representative of the family

Length41.7 m137 ft
Wingspan43.4 m142 ft
Height11.8 m39 ft
Range4,627 km2,498 NMWith a typical passenger load
Cruise speed621 km/h335 ktMach 0.58
Service ceiling9,144 m30,000 ftIt flies above Everest (1.0 times its height)
Maximum take-off weight95,254 kg209,999 lb
Maximum payload54,906 kg121,047 lbIts 160 passengers with baggage would weigh about 16.0 t; the rest is fuel and cargo
Typical capacity160 passengersUp to 178 in a high-density layout
Endurance7 h 27 minAt cruise speed, non-stop

The type first flew in 1959 (67 years ago) · About 39 units built · Production ended in 1965

Figures for the type, not for this particular aircraft: each variant and each configuration changes something. They are shown in both systems used in aviation.

The story of the type

Design and development

In the 1950s, Canadair acquired a licence to build the Bristol Britannia airliner. Their first use of it was to build the heavily modified Canadair CL-28 Argus patrol aircraft (RCAF designation CP-107) that combined the Britannia's wings and tail sections with a new fuselage and engines. The resulting aircraft had lower speed and service ceiling, but it had two bomb bays and greatly extended loiter times.

The RCAF required a replacement for its C-54GM North Star, itself an extensive redesign of the Douglas C-54 Skymaster. Among many changes, the proposed new aircraft was powered by Merlin engines. Canadair began work on a long range transport primarily intended to provide personnel and logistics support for Canadian Forces in Europe. In January 1957 Canadair received a contract for eight aircraft, later increased to 12. The RCAF designation for the new design was CC-106 Yukon, while the company's civilian variant was known as the CL-44-6. In company parlance the CL-44 was simply "the Forty-Four."

The RCAF specified the CL-44 to be equipped with Bristol Orion engines. When the British Ministry of Supply canceled the Orion program, the RCAF revised the specifications to substitute the Rolls-Royce Tyne 11. The CL-44 fuselage was lengthened, making it 12 ft 4 in (3.75 m) longer than the Britannia 300 with two large cargo doors added on the port side on some aircraft, while the cabin was pressurised to maintain a cabin altitude of 2,400 m at 9,000 m (30,000 ft). The design used modified CL-28 wings and controls. The Yukon could accommodate 134 passengers and a crew of nine. In the casualty evacuation role, it could take 80 patients and a crew of 11.

The rollout of the Yukon was a near-disaster because the prototype could not be pushed out of the hangar since the vertical fin could not clear the hangar doors. The first flight took place 15 November 1959 at Cartierville Airport. During test flights many problems were encountered, from complete electrical failure to engines shaking loose and almost falling off. Rolls-Royce had problems delivering engines, resulting in the sarcastically named "Yukon gliders" being parked outside Canadair as late as 1961.

Operational history

Initially, the CL-44-6 was produced for the RCAF as the CC-106 Yukon. Once initial problems were resolved, in RCAF service the Yukon performed well and in December 1961, a Yukon set a world record for its class when it flew 6,750 mi (10,860 km) from Tokyo to RCAF Station Trenton, Ontario, in 17 hours, three minutes at an average speed of 400 mph (640 km/h). Later, a Yukon set a new record staying airborne for 23 hours and 51 minutes. These records were unbroken until bettered by the Boeing 747SP in 1975. By the time of their retirement, Yukons had flown 65 million miles, 1.5 billion passenger miles and 360 million ton-miles.

The CL-44D4 was briefly considered for purchase by the United States Air Force in the 1960s but the project was never culminated due to political backlash in Canada and the United States. The USAF purchase of the CL-44 was complicated by two factors. It came in the aftermath of the cancellation of the Avro Canada CF-105 Arrow and involved a "swap deal" wherein 100 McDonnell F-101 Voodoo fighters were obtained in return for a contract for 232 CL-44-D4 transports for the Military Air Transport Service (MATS). The political controversy that resulted led to problems for a Quebec-based company receiving a contract so soon after an Ontario-based company had lost a major contract. The USAF also quickly found that buying a foreign aircraft was not easy when American companies wanted the business and they relinquished the contract to Canadair, awarding an order to Boeing for the KC-135 Stratotanker.

On the cargo aircraft variant CL-44D4 the entire tail section hinged. It could be opened using hydraulic actuators to load large items quickly. An inflatable seal at the hinge-break enabled cabin pressure to be maintained, and eight hydraulic-operated locks assured structural integrity. The tail could be opened from controls within the tail in 90 seconds. The flight controls at the joint were maintained by a system of push pads.

The CL-44D4 was the first large aircraft to be able to "swing" its tail, although some small naval aircraft had this feature to ease storage. These, however, required rigging before flight. There were only four original customers who bought and operated the CL-44D4.

Loftleiðir was the only passenger operator of the CL-44J, variant of CL-44D4 stretched on request by Canadair. It was the largest passenger aircraft flying over the Atlantic Ocean at that time. Loftleiðir marketed the CL-44J under the name "Rolls-Royce 400 PropJet". This led to the confusion that the CL-44J is sometimes referred to as the Canadair-400. Loftleiðir Icelandic Airlines merged with Air Iceland in 1973 and became today's Icelandair.

The CC-106 Yukons retired in March 1971 and were replaced by the CC-137 (Boeing 707).

Variants

CL-44-6

Version built for the Royal Canadian Air Force as the CC-106 Yukon, 12 built.

CL-44D4-1

Civil, commercial cargo aircraft, civil prototype and production aircraft for Seaboard World Airlines, eight built.

CL-44D4-2

Civil, commercial cargo aircraft originally built for Flying Tiger Line, 13 built.

CL-44D4-6

Civil, commercial cargo aircraft originally built for Slick Airways, four built.

CL-44D4-8

Civil passenger aircraft for Loftleiðir Icelandic, two built.

CL-44J

Four CL-44D4 aircraft stretched by Canadair on request of Icelandic Airlines Loftleiðir, with a section, 10 ft 1 in (3.07 m) forward of the wing, and another section of 5 ft 1in (1.55 m) aft of the wing. This enabled the installation of 29 extra seats, bringing the capacity to 189 passengers. The maximum take-off weight stayed the same since the extra weight was compensated by removing the center wing tanks. Therefore, it can be said that the stretch was a trade of capacity for range.

CL-44-O

Also known as the Skymonster and CL-44 Guppy. The CL-44-O was a single CL-44D4-2 (c/n 16) converted by Conroy Aircraft, who removed the fuselage shell above the floorline, and rebuilt an enlarged fuselage to make it into a Guppy-type aircraft. It was intended to transport Rolls-Royce RB211 engine pods to the United States for Lockheed's L-1011 TriStar. The "O" stood for "outsized fuselage". In the end, the Lockheed L-100 Hercules was used instead.

Overview and history adapted from Wikipedia (CC BY-SA) · technical figures from the manufacturer’s published specifications and standard aviation references

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This page was last updated on October 11, 2026

APA

Vuelopedia. (2026, October 11). Canadair CL-44. Retrieved October 16, 2026, from https://vuelopedia.org/en/model/cl44

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Harvard

Vuelopedia (2026) Canadair CL-44. Available at: https://vuelopedia.org/en/model/cl44 (Accessed: 16 October 2026).

BibTeX

@misc{vuelopedia_en_model_cl44,
  author       = {{Vuelopedia}},
  title        = {{Canadair CL-44}},
  publisher    = {Fundación Poderia},
  year         = {2026},
  date         = {2026-10-11},
  url          = {https://vuelopedia.org/en/model/cl44},
  howpublished = {\url{https://vuelopedia.org/en/model/cl44}},
  urldate      = {2026-10-16},
  note         = {Accessed 2026-10-16}
}

Wikipedia

{{cite web |url=https://vuelopedia.org/en/model/cl44 |title=Canadair CL-44 |website=Vuelopedia |publisher=Fundación Poderia |date=2026-10-11 |access-date=2026-10-16 |language=en}}

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