Bombardier Challenger 600 series#CL-605

{{Short description|Business jet family by Canadair, later Bombardier}}

{{Redirect|Canadair Challenger||Bombardier Challenger (disambiguation)}}

{{Use Canadian English|date=November 2021}}

{{Use dmy dates|date=November 2021}}

{{Infobox aircraft

|name = Challenger 600/601/604/605/650

|image = File:OH-WII CL604 pvt (7950005490).jpg

|caption = A Bombardier CL-604

|type = Business jet

|manufacturer = Canadair
Bombardier Aerospace

|designer=

|first_flight= 8 November 1978

|introduction=

|retired=

|status = In production

|primary_user=

|more_users=

|produced= 1980–present

|number_built= 1,066 (October 2018){{cite news |url=https://www.flightglobal.com/news/articles/nbaa-business-jet-designs-that-changed-the-industry-452471/ |title=NBAA: Business jet designs that changed the industry |date=12 October 2018 |author=Murdo Morrison |work=FlightGlobal}}

|variants=

|developed_into= Bombardier CRJ100/200
Bombardier Global Express

}}

The Bombardier Challenger 600 series is a family of business jets developed by Canadair after a Bill Lear concept, and then produced from 1986 by its new owner, Bombardier Aerospace.

At the end of 1975, Canadair began funding the development of LearStar 600, and then bought the design for a wide-cabin business jet in April 1976.

On 29 October, the programme was launched, backed by the Canadian federal government, and designed to comply with new FAR part 25 standards.

In March 1977, it was renamed the Challenger 600 after Bill Lear was phased out, and the original conventional tail was changed for a T-tail among other developments.

The first prototype was rolled out on 25 May 1978, and performed its maiden flight on 8 November.

The flight test program saw a deadly crash on 3 April 1980, but Transport Canada approved the CL-600 type certification on 10 August 1980.

In 1986, Canadair was close to bankruptcy and was bought by Bombardier.

The jet was later stretched into the Bombardier CRJ regional airliner, introduced on 19 October 1992, and the longer range Global Express, introduced in July 1999.

The 500th Challenger was rolled out in May 2000, and the 1000th was delivered to NetJets in December 2015.

By October 2018, 1,066 aircraft had been built.

The Challenger is a low-wing jet powered by two turbofans mounted in aft fuselage pods, with a supercritical wing and a stand-up cabin with two seating sections.

The original Lycoming ALF 502 turbofans were replaced by a pair of General Electric CF34s on the CL-601, which also gained winglets, and first flew on 10 April 1982.

Subsequent variants have updated systems, avionics, and higher weights.

Development

=Origins=

File:Learstar-600.jpg

Around 1974, American aviation inventor Bill Lear conceptualised the LearStar 600, a low-wing, long-distance business jet, which was powered by a pair of Garrett TFE731-1 geared turbofan engines and equipped with a supercritical wing.{{cite magazine |author= Mike Hirst |url= https://www.flightglobal.com/pdfarchive/view/1978/1978%20-%201521.html |title= Challenger |magazine= Flight International |date= 12 August 1978 |pages= 470–478}} Lear lacked the capabilities to launch such an aircraft, thus sought out other agencies to collaborate with to both produce and sell it, including the Canadian aerospace manufacturer Canadair. According to authors Ron Picklet and Larry Milberry, Canadair's top management were of the opinion that Lear's concept was sketchy at best.Pickler, Ron and Larry Milberry. Canadair: The First 50 Years. Toronto: CANAV Books, 1995. {{ISBN|0-921022-07-7}}. p. 263. Lear did not have an expert grasp of aeronautical engineering; so far, he had only been able to pay an American aeronautical consultant to undertake very preliminary design explorations.Logie, Stuart. Winging it: The Making of Canadair's Challenger. Toronto, Ontario: Macmillan Canada. 1992. {{ISBN|0-77159-145-4}}, p. 55-57.

Following a study, contrasting the proposed Learstar against rivals such as the Lockheed Jetstar, Dassault Falcon 50, and Grumman Gulfstream II, Canadair decided to give its backing to the idea near the end of 1975. According to aerospace industry publication Flight International, the programme was viewed by many Canadians as a step towards developing a privately driven high-technology aviation industry that would compete at a global level. Perhaps more importantly, the Canadian government had issued a demand that Canadair become self-sufficient, thus the company wanted to depend less upon subcontracting arrangements with other firms, such as France's Dassault Aviation and America's Boeing, or providing support packages for existing aircraft for which they had already ended production, such as the CF-5 fighter. Canadair felt a need to prove its ability to independently develop original high-tech projects at this time.

Canadair planned to use Lear's name and skills at self-promotion to secure extensive financial guarantees for a business-jet project from the Canadian federal government. This proved an effective choice: Future Prime Minister Jean Chrétien specifically refers to the effect of personal contact with Lear on his decision to direct financial support to Canadair's program.Low, Stephen. Challenger: An Industrial Romance [http://www.nfb.ca/film/challenger_an_industrial_romance/ (16 mm, 57 min 23, sound, colour film).] Montreal: The National Film Board of Canada, 1980. At the time of these events, Chrétien was successively president of the Treasury Board, minister of Industry, Trade, and Commerce, and minister of Finance, in the Canadian government. Due to the use of letters of comfort, the extent of the ministry's financial commitments for Canadair could be kept from parliament and the public for several years.Report of the Auditor General of Canada to the House of Commons for the fiscal year ended March 31, 1982, para. 10.95 to 10.100. These financial guarantees were later used as an academic example of insufficient monitoring and lax controls in government support of industry.Borins, Stanford F. and Lee Brown. Investments in Failure. New York: Raven Press, 1987. {{ISBN|0-458-80340-5}}.

In April 1976, Canadair acquired the LearStar 600 concept. By then it was {{cvt|63|ft|m}} long, and {{cvt|53.3|ft|m}} wide, and capable of a maximum speed of Mach 0.85 and a range of {{cvt|7,240|km|nmi}}. As an executive jet, it had sufficient capacity for 14 passengers. In a freighter configuration, it had a 3,400 kg (7,500 lb) payload capacity, loaded and unloaded through a forward door. As a commuter airliner, it could seat up to 30 passengers in a 2–1 seating configuration. Canadair developed the design into a large airframe, furnished with a new supercritical wing design, new avionics and engines, as well as for compliance with new FAR part 25 standards. The configuration was frozen in August and a 1/25 model was tested in the National Aeronautical Establishment transonic wind tunnel. Reportedly, in excess of 1,800 hours of wind tunnel testing were performed upon the supercritical wing alone.

=Launch=

Backed by the federal government, the programme was launched on 29 October 1976 with firm orders and deposits for 53 aircraft. Within the next two years, roughly 2,500 employees were involved in designing the aircraft. Changes to the original Learstar configuration had been made on the run up to the launch, such as the conventional tailplane being substituted for a T-tail counterpart after the former was found to be in the path of the engine's exhaust flow, the relocation of fuel storage to the wings, and multiple increases of the aircraft's gross weight. Following disagreements over the direction of the programme, Bill Lear was phased out of involvement. In March 1977, the aircraft was renamed the Challenger 600. Reportedly, following his disassociation with the venture, Lear referred to Canadair's revised design as Fat Albert. Following Lear's death in May 1978, Canadair paid an estimated $25 million to his estate for his contribution to the programme.

Due to the expansion of the design, the original powerplant configuration became untenable. Engine manufacturer Lycoming proposed developing a new model, the Lycoming ALF 502L, which Canadair's design team accepted for the enlarged Challenger, and around which drew up its general arrangement. The type's wide cargo door had been designed in response to the needs of FedEx, the type's original launch customer, having placed an order for 25 aircraft. FedEx had experienced problems with the General Electric CF34 engines, and favoured the Lycoming ALF 502D, instead. Those later had delivery troubles and lacked performance. Reportedly, FedEx converted most of its orders into the Challenger's stretched version, intending to carry up to 12,500 lb of freight at a time using them. FedEx ultimately opted to cancel its orders due to the US Airline Deregulation Act, and the specific aircraft that were already in production were sold to other customers instead.

By the spring of 1977, Canadair had received over 70 firm orders and had begun constructing three prototypes. A $70 million loan was borrowed from European sources to help finance the programme, which lessened the financial burden on the Canadian government. A full-scale fuselage mockup was displayed at the 1977 Paris Air Show before a European and North American tour. 106 were sold by the end of 1977. In late 1977, in the face of criticism that the project would not be capable of producing an aircraft fulfilling the performance guarantees made, Canadair officials had commented that they expected the first flight to occur in 1978, and that initial deliveries had been scheduled to begin during September 1979. Flight International noted that even prior to the prototype's first flight, the type had already made a noticeable impact upon the competition, including the launch of the Cessna Citation III and Grumman Gulfstream III.

By early March 1978, the first prototype was almost finished and the assembly of the two other had debuted. Destined to control handling qualities and test flight performance, it was formally rolled out on 25 May 1978. 116 orders were confirmed 19 months after go-ahead. By this point, production jigs allowing for a production rate of up to seven Challengers per month had been established, ready for quantity production to proceed. Airframe structural testing began in February 1979. Operational test cycling started in December 1979, simulating 72,638 flight hours by February 1985, while its predicted lifetime was 30,000 hours.

=Flight test phase=

File:Canadair CL-600-1A11 Challenger 600, Bombardier AN1006238.jpg demonstrator.{{cite web |publisher= Canada aviation museum |title= Canadair CL-600 / 601 / 604 Challenger serial 1003, registration C-GCGT |author= Bill Upton |date= 2007 |url= https://documents.techno-science.ca/documents/CASM-Aircrafthistories-CanadairCL-600Challenger.pdf}}]]

On 8 November 1978, the prototype aircraft took off for its maiden flight from Montreal, Quebec. The flight test and certification program were conducted at Mojave Kern County Airport instead of Canada due to better weather. The second and third prototypes first flew during 1979. A test flight on 3 April 1980 in the Mojave Desert resulted in disaster. The aircraft crashed due to the failure of the release mechanism to detach the recovery chute after a deep stall, killing one of the test pilots. The other test pilot and the flight test engineer parachuted to safety.{{Cite web|title=The Crash of Challenger #1001|url=https://www.check-six.com/Crash_Sites/Canadair-CGCGRX.htm|url-status=live|access-date=19 September 2012|website=www.check-six.com|archive-url=https://web.archive.org/web/20101020002420/http://check-six.com/Crash_Sites/Canadair-CGCGRX.htm |archive-date=20 October 2010 }}

The CL-600-1A11 type certification was approved by Transport Canada in August 1980,{{cite web |url= https://wwwapps.tc.gc.ca/saf-sec-sur/2/nico-celn/c_d.aspx?lang=eng&aprv_num=A-131&ISU_NUM=60&START_DATE=2019-11-22&AUTH_DESC=&DESC=&FRGN_NUM=&aprv_type=TA&PARTS_NUM=&id_num=1189 |title= Certificate A-131 |date= 2019-11-22 |publisher= Transport Canada}} and by the US Federal Aviation Administration in November 1980.{{cite web |url= https://rgl.faa.gov/Regulatory_and_Guidance_Library/rgMakeModel.nsf/0/8144c461a8357ac0862584c70081bf7f/$FILE/A21EA_R49.pdf |title= Type Certificate data sheet A21EA |date= November 26, 2019 |publisher= US FAA }}

The program cost was C$1.5 billion (US${{#expr:1.5*90/120round1}} billion at the time).{{cite news |title= Bombardier And The Perils Of Government Interference |date= February 21, 2020 |work= Aviation week |url= https://aviationweek.com/air-transport/editorial-bombardier-perils-government-interference}}

=Further development=

In 1980, the first production model of the Challenger series, the CL-600, entered service with end customers. Early marketing of the type by Canadair typically contrasted the more spacious cabin offered by the Challenger against its competitors, which typically had more narrow fuselages, and therefore cramped conditions, as well as the type's fuel economy. By 1982, while only 10 aircraft had entered service, the company had begun publicising a new model of the aircraft, the CL-601, which was to be powered by a pair of General Electric CF34 turbofan engines in place of the original models’ Lycoming units. On 10 April 1982, the CL-601 performed its maiden flight.{{cite magazine |url= https://www.flightglobal.com/pdfarchive/view/1982/1982%20-%201477.html |title= Canadair announces yet another breakthrough in the fight against the high cost of jet fuel |magazine= Flight International |date= 29 May 1982 |page= 1403}} According to Flight International, the decision to adopt the CF34 engine for the new model was responsible for generating a substantial boom in Challenger sales.

According to Flight International, the slow initial sales of the Challenger heavily contributed to the near-bankruptcy of Canadair, which was only avoided by the purchase of the company by Bombardier in 1986.{{cite news |url= https://www.flightglobal.com/news/articles/opinion-in-praise-of-the-challenger-453872/ |title= OPINION: In praise of the Challenger |work= Flight International |date= 25 November 2018}} Bombardier elected not only to continue production of the type, but also to finance the development of new models and derivatives. This choice was aided by Canadair's design decision to enable the Challenger to be readily stretched from the onset. As of October 2018, the best-selling variant of the Challenger series has been the CL-604, which was launched in 1995. The 500th aircraft was rolled out in May 2000.{{cite news |url= http://aviationweek.com/awin/bombardier-rolls-out-500th-challenger-business-jet |date= 26 June 2000 |title= Bombardier rolls out 500th Challenger business jet |work= Aviation Week Network}} The 1000th, a 650, was delivered to NetJets in December 2015.{{cite news |url= https://www.flightglobal.com/news/articles/netjets-first-challenger-650-enters-operational-ser-420260/ |title= NetJets' first Challenger 650 enters operational service |date= 21 December 2015 |author= Kate Sarsfield |work= Flightglobal}}

According to Flight International, the Challenger 600 has been a foothold in the market for Bombardier, allowing them to more easily develop further business jets, such as the Bombardier Global Express. Another direct derivative of the Challenger series has been the Bombardier CRJ100 series, a larger regional airliner. The publication commented that the Challenger family "appears to have a solid future", observing a production rate of two aircraft per month throughout 2018.

Design

File:Canadair CL-600-2B16 Challenger 605, Bombardier AN1445479.jpg

File:Canadair CC-144B Challenger (CL-600-2A12-601), Canada - Air Force AN0617967.jpg CC-144) has a swept wing, a T-tail and two aft-mounted turbofans]]

The Challenger is a twin-engined business jet, described by Flight International as being a "miniaturised twinjet airliner in every respect". While the Challenger is generally similar in configuration to previous aircraft of its type, some of its features stand out; for example, a widened fuselage allows a "walk-about cabin". The Challenger was also one of the first business jets to be designed with a supercritical wing. The wing was referred to by Canadair as being one of the aircraft's most advanced features. It is also capable of performing short takeoffs while maintaining the speed and comfort levels normally associated with larger jetliners.

The Challenger's wing has been referred to as being a modified NACA symmetrical aerofoil. Akin to other supercritical wings, it features a rounded leading edge, an inverted camber, a blunt trailing edge and scalloping of the underside. The twin-spar wing box structure spans the entire length of the wing and is compartmentalised to form five internal fuel tanks; these tanks can accommodate up to 14,661 lb of fuel, nearly half the aircraft's empty weight.

The skins of the wings are produced using large milling machines, which in 1978 were claimed to be superior to anything else in North America. Many elements, such as the flaps, ailerons, and leading edge, feature conventional construction. Several parts, including the wing/fuselage fairing, flap shrouds, and wingtips, are moulded out of Kevlar, as are other elements of the aircraft.

The original CL-600 Challenger was powered by two Lycoming ALF 502L turbofan engines, which were developed specifically for the Challenger. Subsequent models adopted other powerplants, including the General Electric CF34 engine. The engines are mounted on the rear fuselage close to the aircraft's tail, providing smooth airflow to the engines even when flown at high angles of attack, although this was in a lower position than the original LearStar concept had placed them to mitigate unfavourable pitch control characteristics. The engines are fitted with thrust reversers to decrease landing distances. An auxiliary power unit is also present for starting the engines and providing air conditioning within the cabin while on the ground.

The fuselage comprises three sections — the nose, centre, and tail — which are manufactured separately in their own jigs and joined later on in the production process. It has been designed to be pressurised at a maximum differential of 9.3 lb/sq in. Various cutouts are present across the fuselage to accommodate features such as a large main door on the port side of the aircraft forward of the wing, multiple regulation-compliant emergency exits, a baggage hatch on the port-side aft of the wing, and numerous windows.

The fuselage diameter was designed to accommodate an unobstructed cabin floor, a cabin height of 6 ft 1 in in the centre section, and space for the wing box, underfloor integral fuel tanks, air ducts, and various control cabling. It was also designed to easily accommodate Canadair's early plans to stretch the fuselage, for which equal-length plugs are installed fore and aft of the centre section to greatly increase the Challenger's capacity.

Various avionics are present in the Challenger. As standard, the CL-600 is furnished with a dual-channel Sperry SPZ-600 automatic flight control system, incorporating a flight director and air data computers; more typical to larger commercial aircraft, this system is certifiable for conducting Category 3A automatic landings. The flight control system features significant redundancy, including three individual hydraulic systems; even with complete failure and the loss of one actuator, a viable level of assisted control over the key flight surfaces remains present. Weather radar and Marconi-built solid-state instrument displays are supplied as standard, as well as a Collins-built radio set; optional long-range, radio-based equipment, such as a HF radio set and VHF navigational aids can be installed.

In a standard executive aircraft configuration, the cabin is divided between the forward galley, and two seating sections, which are typically fitted with a four-chair club section followed by either a conference grouping area or divans, along with a lavatory at the aft end. The chairs are fully reclining and can swivel, while the divans can serve as sleeping accommodation. Early examples feature luxuries such as telephones, lighting controls, and stereo systems; foldaway tables attached to the cabin walls were also installed, along with a pair of wardrobes, one fore and one aft, for storing hand luggage and other small items.

Variants

=Challenger 600 (CL-600-1A11) =

;CL-600: Original production version, powered by Lycoming ALF 502L turbofans with {{Convert|7500|lbf|abbr=on}} of thrust each, 81 built from 1978 to 1982

;CL-600S: CL-600 with the winglets introduced on the CL-601-1A, three built

;Canadair CC-144: Twelve aircraft were purchased by the Royal Canadian Air Force and delivered in 1982, including the CE-144 and CX-144.{{cite news |url= https://www.flightglobal.com/news/articles/pictures-four-decades-of-the-challenger-600-series-452536/ |title= PICTURES: Four decades of the Challenger 600 series |work= Flight International |date= 10 October 2018}} A further seven airframes have been procured from 1982 to 2020. Models CL-600, CL-601, CL-604, and CL-650 have all been procured to fill the role.

;Canadair CE-144: Three electronic warfare (EW) trainers were converted to/from basic CC-144.

;Canadair CX-144: Second prototype, a CL-600-1A11, c/n 1002, was allocated to the RCAF after finishing its test programme. Used at the Aerospace Engineering and Test Establishment (AETE), CFB Cold Lake until retirement in 1993, it is now preserved at the CFB Winnipeg, designated CC-144 in service.

=Challenger 601-1A (CL-600-2A12)=

; CL-601-1A: A refined version with winglets to decrease drag and more powerful General Electric CF34-1A turbofans (66 built, including six Canadian Forces CC-144Bs).{{cite web |last=Walker |first=R.R. |url=http://rwrwalker.ca/CF_Challenger_detailed.html |title=CC-144 Challenger detailed list |website=Canadian Military Aircraft Serial Numbers, Canadian Armed Forces |date=2006 |access-date=September 19, 2012}}

; CL-601-1A/ER: 601-1A with additional fuel tank in the tail

=Challenger 601-3A/3R (CL-600-2B16)=

File:Canadair CL-600-2A12 Challenger 601 AN2214078.jpgs.]]

;CL-601-3A: Equipped with General Electric CF34-3A turbofans with a higher flat rating and a glass cockpit. First version marketed by Bombardier.

;CL-601-3A/ER: 601-3A with additional fuel tank in the tail

;CL-601-3R: Equipped with General Electric CF34-3A1 turbofans, tail tank made standard

=Challenger 604/605/650=

File:VH-URR Bombardier CL-600-2B16 Challenger 604 (6485923771).jpg

;{{visible anchor|CL-604}}: Equipped with General Electric CF34-3B turbofans, added saddle tanks for increased fuel capacity, new undercarriage for higher takeoff and landing weight; structural improvements to wings and tail, new Rockwell Collins Pro Line 4 avionics system

;CL-604 MMA: (Multi-Mission Aircraft), militarized version, developed by Field Aviation,[http://www.casr.ca/id-arcticviking-challenger.htm "Update: Denmark's Arctic Assets and Canada's Response — Danish Air Force Aircraft on a Mission over Canada's High Arctic."] {{webarchive|url=https://web.archive.org/web/20090709185835/http://www.casr.ca/id-arcticviking-challenger.htm |date=2009-07-09 }} Canadian American Strategic Review,July 2009. Retrieved: September 19, 2012. in Danish service. The aircraft are employed on maritime patrol and search and rescue missions. They are capable of landing on the short, rough, gravel airstrips common in the Arctic.

;C-143A: A single Challenger 604 aircraft was acquired by the United States Coast Guard in December 2005 as its new medium-range command-and-control aircraft.Parsch, Andreas. [http://www.designation-systems.net/usmilav/412015-L(addendum).html#_Note_C143A "DOD 4120.15-L – Addendum."] designation-systems.net, 2011. Retrieved: September 19, 2012.

Built from 1996 through 2006, over 360 were delivered. Early ones were selling for $4.0–$4.5 million and late models for less than $8 million in 2016.

With {{cvt|27,000 to 27,100|lb}} operating empty weights, it carries six or seven passengers and full fuel with the increased MTOW. It is able to cruise for 7.5–8.0 hrs at Mach 0.80 and to fly five passengers 4,000 nm at Mach 0.74 up to FL 410.

Thrust lapse as altitude increases, hefty power, and wing loadings affects hot-and-high performance. It takes off in {{cvt|3,500 to 4,000|ft}} for under {{cvt|800|nmi}} missions, in {{cvt|5,684|ft}} at MTOW and sea level. In {{cvt|9,123|ft}} at ISA+20C and {{cvt|5,000|ft}} altitudes, TOW is reduced to {{cvt|47,535|lb}} to meet climb requirements.

Pro Line 4 avionics include six {{cvt|7.25|in|cm}} cathode-ray tubes and dual Flight management systems.

It burns {{cvt|3,800|lb}} in the first hour, {{cvt|3,200|lb}} in the second hour, {{cvt|2,800|lb}} in the third hour then {{cvt|2,000|lb}}/hr.

Scheduled maintenance is done every 200 h or six months, and major inspections are made every 96 months, and includes $110,000 landing-gear overhauls, the {{cvt|8,729|lbf|kN}} CF34-3B turbofans cost $375 per engine per hour.{{cite news |url= http://aviationweek.com/business-aviation/used-aircraft-report-challenger-604 |title= Used Aircraft Report: Challenger 604 |date= Aug 25, 2016 |author= Fred George |work= Business & Commercial Aviation |publisher= Aviation Week}}

File:Canadair CL-600-2B16 Challenger 605, Bombardier AN1426362.jpg capability and even larger screens.]]

;CL-605: Following a first flight in January 2006,{{cite press release |url=https://bombardier.com/en/media/news/bombardier-challenger-605-executes-flawless-first-flight|date=January 23, 2006|title=Bombardier Challenger 605 Executes Flawless First Flight|work=Bombardier}} the Challenger 605 was certified and introduced in early 2006. Compared to the Challenger 604, the airframe was updated with larger cabin windows and a new tail cone, and the flight deck was updated with the Collins Pro Line 21 system with electronic flight bag capability. The 200th Challenger 605 entered service in October 2012.{{cite press release|url=https://bombardier.com/en/media/news/bombardiers-200th-challenger-605-jet-enters-service|date=October 31, 2012|title=Bombardier's 200th Challenger 605 Jet Enters Service|work=Bombardier}}

;CL-605 MSA: A maritime patrol aircraft design under development by Boeing.Hemmerdinger, Jon. [http://www.flightglobal.com/news/articles/boeing39s-challenger-based-maritime-surveillance-aircraft-nears-first-394743/ "Boeing's Challenger-based maritime surveillance aircraft nears first flight."] flightglobal.com, January 10, 2014. Retrieved: January 16, 2016. Boeing has proposed a repackaging of some of the Boeing P-8 Poseidon sensors but not weapons into a less expensive airframe, the Bombardier Challenger 605 business jet.Gates, Dominic. [http://seattletimes.com/html/businesstechnology/2023057059_boeingmsaxml.html "Boeing's cheaper surveillance aircraft takes first flight."] Seattle Times (seattletimes.com), March 5, 2014. Retrieved: January 16, 2016. This aircraft is named Maritime Surveillance Aircraft (MSA) and has been depicted with the AN/APY-10 radar, an electro-optical sensor in a retractable turret, and a magnetic anomaly detector.[http://www.casr.ca/ai-boeing-msa-challenger.htm "Maritime Surveillance Aircraft: Boeing selects a Bombardier 'Bizjet', the Challenger 605, as the preferred airframe for its proposed MSA."] {{webarchive|url=https://web.archive.org/web/20130923070241/http://www.casr.ca/ai-boeing-msa-challenger.htm |date=2013-09-23 }} Canadian American Strategic Review, July 2013. Retrieved: January 16, 2015. In February 2014, a MSA demonstrator, which is a modified CL-604, made its first flight. The final aircraft will use the CL-605 airframe.[http://boeing.mediaroom.com/Boeing-Selects-Bombardier-Business-Jet-for-Maritime-Surveillance-Aircraft-Program "Boeing Selects Bombardier business jet for Maritime Surveillance Aircraft Program."] Boeing boeing.mediaroom.com, November 18, 2013. Retrieved: January 16, 2016.[http://www.aviationtoday.com/av/military/Boeings-MSA-Demonstrator-Proves-Airworthy_81556.html "Boeing's MSA demonstrator proves airworthy."] {{Webarchive|url=https://web.archive.org/web/20140306014120/http://www.aviationtoday.com/av/military/Boeings-MSA-Demonstrator-Proves-Airworthy_81556.html |date=6 March 2014 }} Aviation Today (Access Intelligence, LLC.), March 5, 2014. Retrieved: January 16, 2016. The demonstrator currently has the external shapes for the sensors and communications systems which will be added later. The final MSA is expected to cost $55 million to $60 million per aircraft.Hemmerdinger, Jon. [http://www.flightglobal.com/news/articles/field-aviation-achieves-first-flight-of-boeing39s-maritime-surveillance-396659/ "Field Aviation achieves first flight of Boeing's Maritime Surveillance Aircraft.'] flightglobal.com (Reed Business Information), March 5, 2014. Retrieved: January 16, 2016.

The 605 and 650 improve the avionics and cabin, but their performance figures are similar to the 604.

File:Bombardier Aerospace, N650BA, Bombardier Challenger 650 (31378963128).jpg

=Challenger 650=

;Challenger 650: Following a first flight in 2015, the Challenger 650 was certified and introduced in 2015.{{cite press release|url=https://bombardier.com/en/media/news/bombardiers-challenger-650-business-aircraft-receives-easa-certification|date=March 8, 2016|title=Bombardier's Challenger 650 Business Aircraft Receives EASA Certification|work=Bombardier}} Compared to the Challenger 605, it has a redesigned interior cabin, Rockwell Collins Pro Line 21 Advanced avionics, similar to the Challenger 350, Synthetic vision system (SVS) and a 5% increase in takeoff thrust.{{cite news |url= http://aviationweek.com/nbaa2014/bombardier-refreshes-challenger-605-650 |title= Bombardier refreshes Challenger 605 as 650 |work= Aviation Week |author= John Morris |date= Oct 19, 2014 |access-date= 28 September 2015 |archive-date= 29 September 2015 |archive-url= https://web.archive.org/web/20150929115212/http://aviationweek.com/nbaa2014/bombardier-refreshes-challenger-605-650 |url-status= dead }} In 2023, its equipped price was $33M.{{cite news |url= https://infogram.com/bca-table-2023-jets-1ho16vorwrp8x4n |title= Purchase planning handbook - Jets table |date= Second Quarter 2023 |work= Business & Commercial Aircraft}}

Operators

{{More citations needed section|date=June 2020}}

The 500th unit was rolled out in May 2000.{{cite news|url=http://aviationweek.com/awin/bombardier-rolls-out-500th-challenger-business-jet|date=June 26, 2000|title=Bombardier rolls out 500th Challenger business jet|work=Aviation Week Network}}

The 1000th, a 650, was delivered to NetJets in December 2015.{{cite news|url=https://www.flightglobal.com/news/articles/netjets-first-challenger-650-enters-operational-ser-420260/|title=NetJets' first Challenger 650 enters operational service|date=21 December 2015|author=Kate Sarsfield|work=Flightglobal}}

Including the Challenger 300 and Challenger 850, the 1,600 Bombardier Challengers in-service had logged 7.3 million hours and over 4.3 million flights by early 2017.{{cite press release |url= http://www.businessaircraft.bombardier.com/en/news-events/bombardier-business-aircraft%E2%80%99s-service-centre-network-celebrates-completion-over-200-96 |title= Bombardier Business Aircraft's Service Centre Network Celebrates Completion of over 200 96-Month Inspections on Challenger Jets |date= 17 January 2017 |publisher= Bombardier}}

As of December 2017, close to 1,100 Challenger 600 Series have been delivered.{{cite press release |url= http://www.bombardier.com/en/media/newsList/details.bba_20171205_bombardiers-newest-challenger-jet-models-surpass-si.bombardiercom.html |title= Bombardier's Newest Challenger Jet Models Surpass Significant Delivery Milestones |date= 6 December 2017 |publisher= Bombardier}}

By October 2018, the global Challenger fleet amounted to 997: of these, 611 were based in North America, 151 in Europe, 93 in Latin America, 78 in Asia-Pacific, 37 in Africa and 23 in Middle East.{{cite news |url= https://www.flightglobal.com/news/articles/analysis-challenger-600-marks-40-years-in-business-452069/ |title= ANALYSIS: Challenger 600 marks 40 years in business |date= 4 October 2018 |author= Max Kingsley Jones |work= Flightglobal}}

=Military and government operators=

File:ВООПК встреча Королевы Дании (2).jpg welcomed by a Russian Army Orchestra]]

{{Columns-list|colwidth=30em|

;{{AUS}}

;{{CAN}}

;{{CHN}}

;{{CRO}}

;{{CZE}}

;{{DEN}}

;{{FIN}}

  • Finnish Border Guard: two Challenger 650 ordered in 2024 {{cite web | url=https://www.navalnews.com/naval-news/2024/06/finland-orders-new-maritime-surveillance-aircraft/ | title=Finland Orders New Maritime Surveillance Aircraft | date=28 June 2024 }}

;{{GER}}

;{{HKG}}

;{{KOR}}

  • Korea Coast Guard: operates one CL-604 (B701), outfitted for maritime patrol.[http://www.airliners.net/photo/South-Korea--/Canadair-CL-600-2B16-Challenger/1877415/L/ "Picture of the Canadair CL-600-2B16 Challenger 604 aircraft."] airliners.net. Retrieved: October 6, 2012.

;{{PAK}}

;{{SUI}}

  • Swiss Air Force: Two CL-604 bought from REGA for air-ambulance duties.{{cite magazine |last=van der Mark |first=Kees |title=Swiss Air Force Challengers |magazine=Air International |date=August 2019 |volume=97 |issue=2 |page=6 |issn=0306-5634}}

;{{UAE}}

  • United Arab Emirates Air Force: 1 Challenger 650 ordered in February 2019.{{cite web|last=Martin|first=Jeff|title=United Arab Emirates Air Force to buy new special mission aircraft|url=https://www.defensenews.com/digital-show-dailies/idex/2019/02/20/united-arab-emirates-air-force-to-buy-new-special-mission-aircraft|website=Defense News|access-date=20 February 2019|archive-url=https://archive.today/20190220211108/https://www.defensenews.com/digital-show-dailies/idex/2019/02/20/united-arab-emirates-air-force-to-buy-new-special-mission-aircraft/|archive-date=20 February 2019|location=Abu Dhabi|date=20 February 2019|url-status=live}}

;{{USA}}

  • United States Army: 2 Challenger 650 ‘ARTEMIS’ ISTAR introduced 2020{{Cite web|url=https://theaviationist.com/2020/09/27/the-u-s-armys-first-ever-manned-isr-artemis-jet-has-carried-out-missions-over-georgia-and-abkhazia/|title = The U.S. Army's First Ever Manned ISR ARTEMIS Jet Has Carried Out Missions over Georgia and Abkhazia|date = 27 September 2020}}
  • United States Coast Guard: 1 CL-604 (retired 2011) designated as the C-143A Medium Range Command and Control Aircraft (MRC2A), provided VIP transport for high-ranking members of the Department of Homeland Security and U.S. Coast Guard[http://www.uscg.mil/airstaDC/history.asp "History of Air Station Washington."]USCG. Retrieved: September 19, 2012.{{cite web | url=https://cgaviationhistory.org/aircraft_/tkc-aerospace-c-143a-challenger/ | title=TKC Aerospace C-143A "Challenger" (2005) }}
  • FAA / United States Air Force: 3 Challenger CL-600 Jets designated C-143B owned by the FAA and jointly operated with the USAF{{cite web | url=https://www.airandspaceforces.com/weapons-platforms/c-143/ | title=C-143 Combat Flight Inspection Archives }}

}}

=Civilian operators=

File:RCEvacFlight.JPG after the 2011 Tōhoku disaster by Rega]]

File:Bombardier CL-600-2B16 Challenger 605, Qatar Executive JP6749742.jpg]]

File:Aircraft OE-IPZ.jpg]]

{{Columns-list|colwidth=30em|

; {{ALG}}

;{{AUS}}

;{{CAN}}

  • Chartright Air Inc operates two CL-601s, three CL-604s, one CL605 and one CL650.
  • Shaw Communications: operates 2 CL604s.
  • Sunwest Aviation: operates two CL604s.
  • VIH Execujet: operates one CL604.{{Cite web|url=http://www.vihexecujet.com/challenger/|title=Private Jet Charter In Victoria BC On Vancouver Island Canada|website=VIH Execujet|language=en-US|access-date=2019-11-01}}

;{{CRO}}

;{{IND}}

  • Gujarat operates one CL650 for state executive travel.{{Cite web|url=https://www.indiatvnews.com/news/india/gujarat-cm-vijay-rupani-new-rs-191-crore-aircraft-bombardier-challenger-650-561747|title='Bombardier Challenger 650': New Rs 191-crore aircraft to carry Gujarat CM, other VIPs|date=6 November 2019}}

;{{JOR}}

;{{MAS}}

;{{PAK}}

  • Princely Jets: operates one C604 and one C601-3R

;{{QAT}}

;{{CHE}}

;{{THA}}

;{{TUR}}

;{{TKM}}

  • Turkmenistan Airlines for government VIPs. Operates two CL-605's{{cite web |url=http://www.turkmenairlines.com/en/aircraft-fleet |title=Aircraft fleet |website=Turkmenistan Airlines |url-status=dead |archive-url=https://web.archive.org/web/20130822072944/http://www.turkmenairlines.com/en/aircraft-fleet |archive-date=August 22, 2013}}

;{{UAE}}

;{{UK}}

; {{USA}}

}}File:C-FTBZ Canadair Challenger CL.604 (9143358514).jpg 2000 crash remains]]

Incidents and accidents

{{See also|Category:Accidents and incidents involving the Bombardier Challenger 600 series}}

By May 2019, the Challenger fleet suffered 18 hull loss accidents, causing 39 fatalities.{{cite web |url= https://aviation-safety.net/database/types/Canadair-CL-600-Challenger/statistics |title= Canadair Challenger Statistics |work= Aviation Safety Network |publisher= Flight Safety Foundation |date= 6 May 2019}}

class="wikitable sortable"
DateLocation

!Variant

{{abbr|Fat.|Fatalities}}{{abbr|Surv.|Survivors}}Notes
{{nowrap|2000-10-10}}United States, Kansas, Wichita Airport

|CL-600-2B16 Challenger 604

30Test flight, impact with terrain during initial climb and post impact fire{{cite web |url=http://asndata.aviation-safety.net/reports/US/20001010-0_CL60_C-FTBZ.pdf |title=NTSB Aircraft Accident Brief. |archive-url=https://web.archive.org/web/20160108174359/http://asndata.aviation-safety.net/reports/US/20001010-0_CL60_C-FTBZ.pdf |archive-date=2016-01-08 |website=aviation-safety.net |url-status=dead |access-date=January 16, 2016}}
2002-01-04

|United Kingdom, Birmingham International Airport

|CL-600-2B16 Challenger 604

|5

|0

|Rolled rapidly on takeoff and caught fire{{Cite web |title=CL60, Birmingham UK, 2002 {{!}} SKYbrary Aviation Safety |url=https://skybrary.aero/accidents-and-incidents/cl60-birmingham-uk-2002 |access-date=2024-08-01 |website=skybrary.aero}}

2004-11-28United States, Colorado, Montrose Airport

|CL-600-2A12

33Crashed during an attempted takeoff due to icing on airframe{{Cite web |title=CL60, Montrose USA, 2004 {{!}} SKYbrary Aviation Safety |url=https://skybrary.aero/accidents-and-incidents/cl60-montrose-usa-2004 |access-date=2024-08-01 |website=skybrary.aero}}
2005-11-11

|United Kingdom, London Heathrow

|CL-600-2B16 Challenger 604

|0

|5

|Autopilot pitch trim failed and stabiliser trim system failed due to electrical shorting, caused by fault in the design of the Horizontal Stabiliser Trim Control Unit{{Cite web |title=Summary: AAR 1/2008 Bombardier CL600-2B16 Challenger 604, VP-BJM, 11 November 2005 |url=https://www.gov.uk/aaib-reports/summary-aar-1-2008-bombardier-cl600-2b16-challenger-604-vp-bjm-11-november-2005 |access-date=2024-08-01 |website=GOV.UK |language=en}}

2014-01-05United States, Colorado, Aspen Airport

|CL-600-2B16 Challenger 601-3R

12Pilot error crash after tailwind landing in low-level windshear and gust conditions after a go-around.{{Cite web|url=https://aviation-safety.net/database/record.php?id=20140105-1|title=ASN Aircraft accident Canadair CL-600-2B16 Challenger 601 Aspen Airport|last=Ranter|first=Harro|website=aviation-safety.net|access-date=7 June 2020}}
2017-01-07Oman, above Muscat

|CL-600-2B16 Challenger 604

099,000 ft altitude loss after passing through the wake turbulence from an Airbus A380, written off due to damage after emergency landing{{Cite web|url=https://aviation-safety.net/database/record.php?id=20170107-0|title=ASN Aircraft accident Canadair CL-600-2B16 Challenger 604 D-AMSC Muscat, Oman|last=Ranter|first=Harro|website=aviation-safety.net|access-date=18 May 2017}}
2018-03-11Iran, Zagros Mountains

|CL-600-2B16 Challenger 604

110Crashed after a partial instrument failure, leading to a loss of control{{Cite news|url=https://www.nytimes.com/2018/03/11/world/middleeast/turkish-business-jet-crashes-in-iran.html|title=Turkish Plane Crashes in Iran|access-date=March 11, 2018|newspaper=The New York Times|date=2018-03-11|last1=Erdbrink|first1=Thomas}}

{{Main|2018 Iran Bombardier Challenger crash}}

2019-05-05Mexico, Coahuila

|CL-600-2B16 Challenger 601-3A

130Crashed on its return from Las Vegas, Nevada{{Cite web |url= https://aviation-safety.net/database/record.php?id=20190505-1 |title= Aircraft accident Canadair CL-600-2B16 Challenger 601-3A N601VH Monclava |date= May 6, 2019 |work= Aviation Safety Network}}

{{Main|2019 Coahuila Bombardier Challenger crash}}

2021-07-26United States, California, Truckee Tahoe

|CL-600-2B16 Challenger 605

60Crashed on approach{{cite news |url= https://www.flightglobal.com/business-aviation/challenger-605-business-jet-crashes-in-northern-california/144762.article |title= Challenger 605 business jet crashes in northern California |author= Pilar Wolfsteller |date= 27 July 2021 |work= Flightglobal}}{{cite web|url = https://aviation-safety.net/wikibase/265960 |title= ASN Wikibase Occurrence # 265960 |date=July 26, 2021 | work= Aviation Safety Network}}
2022-01-31

|United Kingdom, London Stansted Airport

|CL-600-2B16 Challenger 604

|0

|6

|During a crosswind, plane made a hard landing, left wingtip hit the runway several times. The nose landing gear failed when the stick pusher activated. There were no injuries.{{Cite web |title=AAIB investigation to Bombardier CL-600-2B16 Challenger 604, N999PX |url=https://www.gov.uk/aaib-reports/aaib-investigation-to-bombardier-cl-600-2b16-challenger-604-n999px |access-date=2024-08-01 |website=GOV.UK |language=en}}

2022-12-30

|Mexico, near Venado, San Luis Potosí

|CL-600S Challenger 600

|2

|0

|Aircraft lost after experiencing uncontrolled descent during positioning flight and "apparently disintegrated"{{Cite web |title=Crash of a Canadair CL-600S Challenger near Venado: 2 killed {{!}} Bureau of Aircraft Accidents Archives |url=https://www.baaa-acro.com/crash/crash-canadair-cl-600s-challenger-near-venado-2-killed |access-date=2024-08-01 |website=www.baaa-acro.com}}

2024-02-09United States, Florida, near Naples Airport

|CL-600-2B16 Challenger 604

23Experienced dual engine failure short of the runway; the pilots attempted to land on Interstate 75, the aircraft was destroyed and consumed by a post-crash fire.{{Cite news |last=Dolan |first=Paul |date=2024-02-09 |title=At least 2 dead after twin-engine plane crashes on I-75 in Collier County |url=https://winknews.com/2024/02/09/plane-crash-i-75-collier-county/ |access-date=2024-02-09 |work=WINK-TV |language=en-US}}{{Cite news |last=Fadulu |first=Lola |date=2024-02-09 |title=Plane Crashes on Florida Highway, Killing 2, Authorities Say |url=https://www.nytimes.com/2024/02/09/us/plane-crash-florida-highway-naples.html |access-date=2024-02-09 |work=The New York Times |language=en-US |issn=0362-4331}}{{Cite web |last=Stimson |first=Brie |date=2024-02-10 |title=Audio released from deadly Florida interstate plane crash: 'We've lost both engines' |url=https://www.foxnews.com/us/audio-released-deadly-florida-interstate-plane-crash-weve-lost-both-engines |access-date=2024-02-11 |website=Fox News |language=en-US}}{{Cite web |title=Accident Bombardier CL-600-2B16 Challenger 604 N823KD |url=https://aviation-safety.net/wikibase/351596 |access-date=2024-02-11 |website=aviation-safety.net}}

{{Main|Hop-A-Jet Flight 823}}

Specifications (Challenger 650)

File:Challeng1.jpg

File:Canadair Challenger 600 (7281327706).jpg

{{Aircraft specs

|prime units?=met

|ref= Bombardier.{{cite web |url= https://businessaircraft.bombardier.com/sites/default/files/Challenger650_EN.zip |title= Challenger 650 Factsheet |publisher= Bombardier |date= 2017 |access-date= 2017-11-07 |archive-url= https://web.archive.org/web/20171107221446/https://businessaircraft.bombardier.com/sites/default/files/Challenger650_EN.zip |archive-date= 2017-11-07 |url-status=dead}}

|crew= Two (captain and first officer)

|capacity=2,200 kg (4,850 lb) and up to 19 passengers

|length m=

|length ft= 68

|length in= 5

|span m=

|span ft= 64

|span in= 4

|height m=

|height ft= 20

|height in= 8

|wing area sqm=

|wing area sqft= 489

|aspect ratio= 8.46

|empty weight kg=

|empty weight lb= 27150

|max takeoff weight kg=

|max takeoff weight lb= 48200

|more general=*Fuel capacity: 9,072 kg (20,000 lb)

  • Cabin: 1.83 m (6 ft) high, 2.41 m (7 ft 11 in) wide

|eng1 name= General Electric CF34-3B

|eng1 type=turbofans

|eng1 number=2

|eng1 kn=

|eng1 lbf= 9,220

|max speed kts=

|max speed kmh=

|max speed mach=0.85

|cruise speed kts=

|cruise speed kmh=

|range km =

|range nmi= 4000

|ceiling m=

|ceiling ft= 41000

|wing loading kg/m2=

|wing loading lb/sqft=

|thrust/weight= 0.38

|more performance=

  • Takeoff: 1,720 m (5,640 ft) (SL, ISA, MTOW)
  • Landing: 732 m (2,402 ft) (SL, ISA, typical)

|avionics=

}}

See also

References

{{Reflist}}