Canadair CL-44


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 , and for commercial operators worldwide.
The aircraft is named after the Canadian territory of Yukon.

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 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.
File:Canadair CL-44 N228SW BOAC RWY 09.63 edited-3.jpg|thumb|right|Loading a Canadair CL-44 at Manchester in 1963 with the fuselage swung open. This aircraft was operated by BOAC on charter from Seaboard World Airlines
File:Canadair CL-44, Slick Airways JP7015730.jpg|thumb|Slick Airways at San Francisco 1963
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 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. 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 from Tokyo to RCAF Station Trenton, Ontario, in 17 hours, three minutes at an average speed of 400 mph. 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. 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. The Yukons might have served longer with the Canadian Forces Air Transport Command but for two factors: the need for an aircraft which could operate as an in-flight refueling tanker, and the chronic shortage and high cost of spares, the latter resulting because the CL-44 had never gone into large-scale production. All Yukons were sold to South American and African operators as they could not be registered in North America or Europe since the FAA refused to certify the original windshields which came from the Bristol Britannia because they did not meet flight crew vision standards. The General Dynamics CV880/990 windshields were compatible enough to be adopted into the flight deck structure, but the cost was prohibitive. The CC-106 had the original Bristol Britannia windshield and, on its retirement from RCAF operations, the cost of conversion was estimated at $250,000.00 per unit, cost alone precluding its use in North America and Europe. In 1974, a special exclusion was granted for the CC-106 for civil operations in Canada.

Variants

;CL-44-6
;CL-44D4-1
;CL-44D4-2
;CL-44D4-6
;CL-44D4-8
;CL-44J
;CL-44-O

Operators

Civilian operators

Four original customers who bought and operated the CL-44D4 were: Seaboard World Airlines, The Flying Tiger Line, Slick Airways and the Icelandic Airlines Loftleiðir. All other operators operated second-hand aircraft.
♠ original operators
The Canadair CL-44 suffered 21 hull loss incidents during its operational history including the following: